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1 | ingob | 1 | /*####################################################################################### |
2 | Flight Control |
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3 | #######################################################################################*/ |
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4 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
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5 | // + www.MikroKopter.com |
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6 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
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2050 | holgerb | 7 | // + Software Nutzungsbedingungen (english version: see below) |
8 | // + der Fa. HiSystems GmbH, Flachsmeerstrasse 2, 26802 Moormerland - nachfolgend Lizenzgeber genannt - |
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9 | // + Der Lizenzgeber räumt dem Kunden ein nicht-ausschließliches, zeitlich und räumlich* unbeschränktes Recht ein, die im den |
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10 | // + Mikrocontroller verwendete Firmware für die Hardware Flight-Ctrl, Navi-Ctrl, BL-Ctrl, MK3Mag & PC-Programm MikroKopter-Tool |
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11 | // + - nachfolgend Software genannt - nur für private Zwecke zu nutzen. |
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12 | // + Der Einsatz dieser Software ist nur auf oder mit Produkten des Lizenzgebers zulässig. |
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1 | ingob | 13 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
2050 | holgerb | 14 | // + Die vom Lizenzgeber gelieferte Software ist urheberrechtlich geschützt. Alle Rechte an der Software sowie an sonstigen im |
15 | // + Rahmen der Vertragsanbahnung und Vertragsdurchführung überlassenen Unterlagen stehen im Verhältnis der Vertragspartner ausschließlich dem Lizenzgeber zu. |
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16 | // + Die in der Software enthaltenen Copyright-Vermerke, Markenzeichen, andere Rechtsvorbehalte, Seriennummern sowie |
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17 | // + sonstige der Programmidentifikation dienenden Merkmale dürfen vom Kunden nicht verändert oder unkenntlich gemacht werden. |
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18 | // + Der Kunde trifft angemessene Vorkehrungen für den sicheren Einsatz der Software. Er wird die Software gründlich auf deren |
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19 | // + Verwendbarkeit zu dem von ihm beabsichtigten Zweck testen, bevor er diese operativ einsetzt. |
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20 | // + Die Haftung des Lizenzgebers wird - soweit gesetzlich zulässig - begrenzt in Höhe des typischen und vorhersehbaren |
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21 | // + Schadens. Die gesetzliche Haftung bei Personenschäden und nach dem Produkthaftungsgesetz bleibt unberührt. Dem Lizenzgeber steht jedoch der Einwand |
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22 | // + des Mitverschuldens offen. |
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23 | // + Der Kunde trifft angemessene Vorkehrungen für den Fall, dass die Software ganz oder teilweise nicht ordnungsgemäß arbeitet. |
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24 | // + Er wird die Software gründlich auf deren Verwendbarkeit zu dem von ihm beabsichtigten Zweck testen, bevor er diese operativ einsetzt. |
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25 | // + Der Kunde wird er seine Daten vor Einsatz der Software nach dem Stand der Technik sichern. |
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26 | // + Der Kunde ist darüber unterrichtet, dass der Lizenzgeber seine Daten im zur Vertragsdurchführung erforderlichen Umfang |
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27 | // + und auf Grundlage der Datenschutzvorschriften erhebt, speichert, verarbeitet und, sofern notwendig, an Dritte übermittelt. |
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28 | // + *) Die räumliche Nutzung bezieht sich nur auf den Einsatzort, nicht auf die Reichweite der programmierten Software. |
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29 | // + #### ENDE DER NUTZUNGSBEDINGUNGEN ####' |
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30 | // + Hinweis: Informationen über erweiterte Nutzungsrechte (wie z.B. Nutzung für nicht-private Zwecke) sind auf Anfrage per Email an info(@)hisystems.de verfügbar. |
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1 | ingob | 31 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
2050 | holgerb | 32 | // + Software LICENSING TERMS |
1 | ingob | 33 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
2050 | holgerb | 34 | // + of HiSystems GmbH, Flachsmeerstrasse 2, 26802 Moormerland, Germany - the Licensor - |
35 | // + The Licensor grants the customer a non-exclusive license to use the microcontroller firmware of the Flight-Ctrl, Navi-Ctrl, BL-Ctrl, and MK3Mag hardware |
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36 | // + (the Software) exclusively for private purposes. The License is unrestricted with respect to time and territory*. |
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37 | // + The Software may only be used with the Licensor's products. |
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38 | // + The Software provided by the Licensor is protected by copyright. With respect to the relationship between the parties to this |
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39 | // + agreement, all rights pertaining to the Software and other documents provided during the preparation and execution of this |
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40 | // + agreement shall be the property of the Licensor. |
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41 | // + The information contained in the Software copyright notices, trademarks, other legal reservations, serial numbers and other |
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42 | // + features that can be used to identify the program may not be altered or defaced by the customer. |
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43 | // + The customer shall be responsible for taking reasonable precautions |
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44 | // + for the safe use of the Software. The customer shall test the Software thoroughly regarding its suitability for the |
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45 | // + intended purpose before implementing it for actual operation. The Licensor's liability shall be limited to the extent of typical and |
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46 | // + foreseeable damage to the extent permitted by law, notwithstanding statutory liability for bodily injury and product |
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47 | // + liability. However, the Licensor shall be entitled to the defense of contributory negligence. |
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48 | // + The customer will take adequate precautions in the case, that the software is not working properly. The customer will test |
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49 | // + the software for his purpose before any operational usage. The customer will backup his data before using the software. |
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50 | // + The customer understands that the Licensor collects, stores and processes, and, where required, forwards, customer data |
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51 | // + to third parties to the extent necessary for executing the agreement, subject to applicable data protection and privacy regulations. |
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52 | // + *) The territory aspect only refers to the place where the Software is used, not its programmed range. |
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53 | // + #### END OF LICENSING TERMS #### |
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54 | // + Note: For information on license extensions (e.g. commercial use), please contact us at info(@)hisystems.de. |
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1 | ingob | 55 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
56 | |||
57 | #include "main.h" |
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1320 | hbuss | 58 | #include "mymath.h" |
1330 | killagreg | 59 | #include "isqrt.h" |
1 | ingob | 60 | |
1352 | hbuss | 61 | unsigned char h,m,s; |
62 | unsigned int BaroExpandActive = 0; |
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1153 | hbuss | 63 | int MesswertNick,MesswertRoll,MesswertGier,MesswertGierBias, RohMesswertNick,RohMesswertRoll; |
1166 | hbuss | 64 | int TrimNick, TrimRoll; |
927 | hbuss | 65 | int AdNeutralNick = 0,AdNeutralRoll = 0,AdNeutralGier = 0,StartNeutralRoll = 0,StartNeutralNick = 0; |
1703 | holgerb | 66 | int Mittelwert_AccNick, Mittelwert_AccRoll; |
1643 | holgerb | 67 | unsigned int NeutralAccX=0, NeutralAccY=0; |
805 | hbuss | 68 | int NaviAccNick, NaviAccRoll,NaviCntAcc = 0; |
1639 | holgerb | 69 | int NeutralAccZ = 0; |
2316 | holgerb | 70 | signed char NeutralAccZfine = 0; |
1683 | killagreg | 71 | unsigned char ControlHeading = 0;// in 2° |
693 | hbuss | 72 | long IntegralNick = 0,IntegralNick2 = 0; |
73 | long IntegralRoll = 0,IntegralRoll2 = 0; |
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74 | long IntegralAccNick = 0,IntegralAccRoll = 0,IntegralAccZ = 0; |
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75 | long Integral_Gier = 0; |
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76 | long Mess_IntegralNick = 0,Mess_IntegralNick2 = 0; |
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77 | long Mess_IntegralRoll = 0,Mess_IntegralRoll2 = 0; |
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78 | long Mess_Integral_Gier = 0,Mess_Integral_Gier2 = 0; |
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79 | long MittelIntegralNick,MittelIntegralRoll,MittelIntegralNick2,MittelIntegralRoll2; |
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1685 | holgerb | 80 | long SummeNick=0,SummeRoll=0; |
1 | ingob | 81 | volatile long Mess_Integral_Hoch = 0; |
1840 | holgerb | 82 | int KompassValue = -1; |
1837 | holgerb | 83 | int KompassSollWert = 0; |
1941 | holgerb | 84 | //int KompassRichtung = 0; |
1839 | holgerb | 85 | char CalculateCompassTimer = 100; |
86 | unsigned char KompassFusion = 32; |
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87 | unsigned int KompassSignalSchlecht = 50; |
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855 | hbuss | 88 | unsigned char MAX_GAS,MIN_GAS; |
1 | ingob | 89 | unsigned char HoehenReglerAktiv = 0; |
880 | hbuss | 90 | unsigned char TrichterFlug = 0; |
395 | hbuss | 91 | long Umschlag180Nick = 250000L, Umschlag180Roll = 250000L; |
693 | hbuss | 92 | long ErsatzKompass; |
2437 | holgerb | 93 | int ErsatzKompassInGrad, CompassCorrected; // Kompasswert in Grad |
693 | hbuss | 94 | int GierGyroFehler = 0; |
1211 | hbuss | 95 | char GyroFaktor,GyroFaktorGier; |
96 | char IntegralFaktor,IntegralFaktorGier; |
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1153 | hbuss | 97 | int DiffNick,DiffRoll; |
2427 | holgerb | 98 | unsigned int StickGasHover = 127; |
99 | int HoverGasMin = 0, HoverGasMax = 1023; |
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1943 | holgerb | 100 | int StickNick = 0,StickRoll = 0,StickGier = 0,StickGas = 0; |
1377 | hbuss | 101 | //int Poti1 = 0, Poti2 = 0, Poti3 = 0, Poti4 = 0, Poti5 = 0, Poti6 = 0, Poti7 = 0, Poti8 = 0; |
1391 | killagreg | 102 | unsigned char Poti[9] = {0,0,0,0,0,0,0,0}; |
1 | ingob | 103 | volatile unsigned char SenderOkay = 0; |
1698 | holgerb | 104 | char MotorenEin = 0,StartTrigger = 0; |
1246 | killagreg | 105 | long HoehenWert = 0; |
106 | long SollHoehe = 0; |
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1942 | holgerb | 107 | signed int AltitudeSetpointTrimming = 0; |
1855 | holgerb | 108 | long FromNC_AltitudeSetpoint = 0; |
109 | unsigned char FromNC_AltitudeSpeed = 0; |
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1862 | holgerb | 110 | unsigned char carefree_old = 50; // to make the Beep when switching |
1942 | holgerb | 111 | signed char WaypointTrimming = 0; |
1840 | holgerb | 112 | int CompassGierSetpoint = 0; |
2009 | holgerb | 113 | unsigned char CalibrationDone = 0; |
2061 | holgerb | 114 | char NeueKompassRichtungMerken = 0; |
1692 | holgerb | 115 | int LageKorrekturRoll = 0,LageKorrekturNick = 0, HoverGas = 0; |
1153 | hbuss | 116 | //float Ki = FAKTOR_I; |
1676 | holgerb | 117 | int Ki = 10300 / 33; |
395 | hbuss | 118 | unsigned char Looping_Nick = 0,Looping_Roll = 0; |
119 | unsigned char Looping_Links = 0, Looping_Rechts = 0, Looping_Unten = 0, Looping_Oben = 0; |
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1 | ingob | 120 | |
121 | unsigned char Parameter_Luftdruck_D = 48; // Wert : 0-250 |
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2342 | holgerb | 122 | unsigned char Parameter_HoehenSchalter = 0; // Wert : 0-250 |
1 | ingob | 123 | unsigned char Parameter_Hoehe_P = 16; // Wert : 0-32 |
124 | unsigned char Parameter_Hoehe_ACC_Wirkung = 58; // Wert : 0-250 |
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125 | unsigned char Parameter_KompassWirkung = 64; // Wert : 0-250 |
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1283 | hbuss | 126 | unsigned char Parameter_Hoehe_GPS_Z = 64; // Wert : 0-250 |
1111 | hbuss | 127 | unsigned char Parameter_Gyro_D = 8; // Wert : 0-250 |
173 | holgerb | 128 | unsigned char Parameter_Gyro_P = 150; // Wert : 10-250 |
1 | ingob | 129 | unsigned char Parameter_Gyro_I = 150; // Wert : 0-250 |
1322 | hbuss | 130 | unsigned char Parameter_Gyro_Gier_P = 150; // Wert : 10-250 |
131 | unsigned char Parameter_Gyro_Gier_I = 150; // Wert : 10-250 |
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1 | ingob | 132 | unsigned char Parameter_Gier_P = 2; // Wert : 1-20 |
133 | unsigned char Parameter_I_Faktor = 10; // Wert : 1-20 |
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134 | unsigned char Parameter_UserParam1 = 0; |
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135 | unsigned char Parameter_UserParam2 = 0; |
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136 | unsigned char Parameter_UserParam3 = 0; |
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137 | unsigned char Parameter_UserParam4 = 0; |
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499 | hbuss | 138 | unsigned char Parameter_UserParam5 = 0; |
139 | unsigned char Parameter_UserParam6 = 0; |
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140 | unsigned char Parameter_UserParam7 = 0; |
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141 | unsigned char Parameter_UserParam8 = 0; |
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2349 | holgerb | 142 | unsigned char Parameter_NickControl = 100; |
1 | ingob | 143 | unsigned char Parameter_ServoNickControl = 100; |
1232 | hbuss | 144 | unsigned char Parameter_ServoRollControl = 100; |
2296 | holgerb | 145 | unsigned char Parameter_ServoNickComp = 50; |
146 | unsigned char Parameter_ServoRollComp = 85; |
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173 | holgerb | 147 | unsigned char Parameter_LoopGasLimit = 70; |
1120 | hbuss | 148 | unsigned char Parameter_AchsKopplung1 = 90; |
149 | unsigned char Parameter_AchsKopplung2 = 65; |
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150 | unsigned char Parameter_CouplingYawCorrection = 64; |
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151 | //unsigned char Parameter_AchsGegenKopplung1 = 0; |
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499 | hbuss | 152 | unsigned char Parameter_DynamicStability = 100; |
921 | hbuss | 153 | unsigned char Parameter_J16Bitmask; // for the J16 Output |
154 | unsigned char Parameter_J16Timing; // for the J16 Output |
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155 | unsigned char Parameter_J17Bitmask; // for the J17 Output |
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156 | unsigned char Parameter_J17Timing; // for the J17 Output |
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1051 | killagreg | 157 | unsigned char Parameter_NaviGpsGain; |
158 | unsigned char Parameter_NaviGpsP; |
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159 | unsigned char Parameter_NaviGpsI; |
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160 | unsigned char Parameter_NaviGpsD; |
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2344 | holgerb | 161 | unsigned char Parameter_NaviGpsA; |
2447 | holgerb | 162 | //unsigned char Parameter_NaviOperatingRadius; |
993 | hbuss | 163 | unsigned char Parameter_NaviWindCorrection; |
164 | unsigned char Parameter_NaviSpeedCompensation; |
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921 | hbuss | 165 | unsigned char Parameter_ExternalControl; |
1916 | holgerb | 166 | unsigned char Parameter_GlobalConfig; |
167 | unsigned char Parameter_ExtraConfig; |
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1966 | holgerb | 168 | unsigned char Parameter_MaximumAltitude; |
1403 | hbuss | 169 | unsigned char Parameter_Servo3,Parameter_Servo4,Parameter_Servo5; |
1668 | holgerb | 170 | unsigned char CareFree = 0; |
1876 | holgerb | 171 | const signed char sintab[31] = { 0, 2, 4, 6, 7, 8, 8, 8, 7, 6, 4, 2, 0, -2, -4, -6, -7, -8, -8, -8, -7, -6, -4, -2, 0, 2, 4, 6, 7, 8, 8}; // 15° steps |
1622 | killagreg | 172 | |
492 | hbuss | 173 | signed int ExternStickNick = 0,ExternStickRoll = 0,ExternStickGier = 0, ExternHoehenValue = -20; |
614 | hbuss | 174 | int MaxStickNick = 0,MaxStickRoll = 0; |
871 | hbuss | 175 | unsigned int modell_fliegt = 0; |
1861 | holgerb | 176 | volatile unsigned char FC_StatusFlags = 0, FC_StatusFlags2 = 0; |
1121 | hbuss | 177 | long GIER_GRAD_FAKTOR = 1291; |
1153 | hbuss | 178 | signed int KopplungsteilNickRoll,KopplungsteilRollNick; |
1209 | hbuss | 179 | signed int tmp_motorwert[MAX_MOTORS]; |
1591 | holgerb | 180 | char VarioCharacter = ' '; |
2028 | holgerb | 181 | unsigned int HooverGasEmergencyPercent = 0; // The gas value for Emergency landing |
2230 | holgerb | 182 | unsigned int GasIsZeroCnt = 0; // to detect that the gas-stick is down for a while |
2309 | holgerb | 183 | signed int Variance = 0; |
184 | signed int CosAttitude; // for projection of hoover gas |
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185 | unsigned char ACC_AltitudeControl = 0; |
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2390 | holgerb | 186 | unsigned char LowVoltageLandingActive = 0; |
2408 | holgerb | 187 | unsigned char LowVoltageHomeActive = 0; |
1591 | holgerb | 188 | |
2367 | holgerb | 189 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
190 | #define OPA_OFFSET_STEP 5 |
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191 | #else |
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192 | #define OPA_OFFSET_STEP 10 |
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193 | #endif |
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194 | |||
1639 | holgerb | 195 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
196 | // Debugwerte zuordnen |
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197 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
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198 | void CopyDebugValues(void) |
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199 | { |
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2373 | holgerb | 200 | DebugOut.Analog[0] = ToNaviCtrl.IntegralNick;//IntegralNick / (EE_Parameter.GyroAccFaktor * 4); |
201 | DebugOut.Analog[1] = ToNaviCtrl.IntegralRoll;//IntegralRoll / (EE_Parameter.GyroAccFaktor * 4); |
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1639 | holgerb | 202 | DebugOut.Analog[2] = Mittelwert_AccNick / 4; |
203 | DebugOut.Analog[3] = Mittelwert_AccRoll / 4; |
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1660 | holgerb | 204 | DebugOut.Analog[4] = (signed int) AdNeutralGier - AdWertGier; |
2367 | holgerb | 205 | DebugOut.Analog[5] = HoehenWert/10; |
2309 | holgerb | 206 | DebugOut.Analog[6] = Aktuell_az;//AdWertAccHoch;//(Mess_Integral_Hoch / 512); |
1639 | holgerb | 207 | DebugOut.Analog[8] = KompassValue; |
208 | DebugOut.Analog[9] = UBat; |
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209 | DebugOut.Analog[10] = SenderOkay; |
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1941 | holgerb | 210 | DebugOut.Analog[11] = ErsatzKompassInGrad; |
1702 | holgerb | 211 | DebugOut.Analog[12] = Motor[0].SetPoint; |
212 | DebugOut.Analog[13] = Motor[1].SetPoint; |
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213 | DebugOut.Analog[14] = Motor[2].SetPoint; |
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214 | DebugOut.Analog[15] = Motor[3].SetPoint; |
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1639 | holgerb | 215 | DebugOut.Analog[20] = ServoNickValue; |
2322 | holgerb | 216 | DebugOut.Analog[21] = HoverGas; |
1639 | holgerb | 217 | DebugOut.Analog[22] = Capacity.ActualCurrent; |
218 | DebugOut.Analog[23] = Capacity.UsedCapacity; |
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2309 | holgerb | 219 | DebugOut.Analog[24] = SollHoehe/10; |
2437 | holgerb | 220 | // DebugOut.Analog[27] = KompassSollWert; |
1682 | holgerb | 221 | DebugOut.Analog[29] = Capacity.MinOfMaxPWM; |
1639 | holgerb | 222 | DebugOut.Analog[30] = GPS_Nick; |
223 | DebugOut.Analog[31] = GPS_Roll; |
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1702 | holgerb | 224 | if(VersionInfo.HardwareError[0] || VersionInfo.HardwareError[1]) DebugOut.Status[1] |= 1; else DebugOut.Status[1] &= 0xfe; |
2373 | holgerb | 225 | //DebugOut.Analog[16] = MinBlTemperture; |
226 | //DebugOut.Analog[17] = MaxBlTemperture; |
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2316 | holgerb | 227 | //DebugOut.Analog[16] = Variance; |
228 | //DebugOut.Analog[17] = VarioMeter; |
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2369 | holgerb | 229 | //DebugOut.Analog[16] = GasIsZeroCnt; |
2316 | holgerb | 230 | //DebugOut.Analog[18] = HoehenWertF; |
231 | //DebugOut.Analog[25] = Parameter_Hoehe_P; |
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232 | //DebugOut.Analog[26] = Parameter_Luftdruck_D; |
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1639 | holgerb | 233 | } |
234 | |||
1760 | holgerb | 235 | |
1232 | hbuss | 236 | void Piep(unsigned char Anzahl, unsigned int dauer) |
1 | ingob | 237 | { |
2263 | holgerb | 238 | unsigned int wait = 0; |
1232 | hbuss | 239 | if(MotorenEin) return; //auf keinen Fall im Flug! |
1966 | holgerb | 240 | GRN_OFF; |
1 | ingob | 241 | while(Anzahl--) |
242 | { |
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1232 | hbuss | 243 | beeptime = dauer; |
2263 | holgerb | 244 | wait = dauer; |
245 | while(beeptime || wait) |
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246 | { |
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247 | if(UpdateMotor) |
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248 | { |
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249 | UpdateMotor = 0; |
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250 | if(!beeptime) wait--; |
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251 | LIBFC_Polling(); |
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252 | }; |
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253 | } |
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1 | ingob | 254 | } |
1966 | holgerb | 255 | GRN_ON; |
1 | ingob | 256 | } |
257 | |||
258 | //############################################################################ |
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1622 | killagreg | 259 | // Messwerte beim Ermitteln der Nullage |
260 | void CalibrierMittelwert(void) |
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261 | //############################################################################ |
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262 | { |
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2426 | holgerb | 263 | // if(PlatinenVersion == 13) SucheGyroOffset(); |
1622 | killagreg | 264 | // ADC auschalten, damit die Werte sich nicht während der Berechnung ändern |
265 | ANALOG_OFF; |
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266 | MesswertNick = AdWertNick; |
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267 | MesswertRoll = AdWertRoll; |
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268 | MesswertGier = AdWertGier; |
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1703 | holgerb | 269 | Mittelwert_AccNick = ACC_AMPLIFY * AdWertAccNick; |
270 | Mittelwert_AccRoll = ACC_AMPLIFY * AdWertAccRoll; |
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1622 | killagreg | 271 | // ADC einschalten |
272 | ANALOG_ON; |
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273 | Umschlag180Nick = (long) EE_Parameter.WinkelUmschlagNick * 2500L; |
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274 | Umschlag180Roll = (long) EE_Parameter.WinkelUmschlagRoll * 2500L; |
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275 | } |
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276 | |||
277 | //############################################################################ |
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1 | ingob | 278 | // Nullwerte ermitteln |
2319 | holgerb | 279 | // Parameter: 0 -> after switch on (ignore ACC-Z fault) |
280 | // Parameter: 1 -> before Start |
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281 | // Parameter: 2 -> calibrate and store ACC |
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282 | unsigned char SetNeutral(unsigned char AdjustmentMode) // retuns: "sucess" |
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1 | ingob | 283 | //############################################################################ |
284 | { |
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2316 | holgerb | 285 | unsigned char i, sucess = 1; |
2367 | holgerb | 286 | unsigned int gier_neutral = 0, nick_neutral = 0, roll_neutral = 0, acc_z_neutral = 0, barotest; |
1702 | holgerb | 287 | VersionInfo.HardwareError[0] = 0; |
2146 | holgerb | 288 | // HEF4017Reset_ON; |
1051 | killagreg | 289 | NeutralAccX = 0; |
1 | ingob | 290 | NeutralAccY = 0; |
291 | NeutralAccZ = 0; |
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2316 | holgerb | 292 | NeutralAccZfine = 0; |
1622 | killagreg | 293 | |
1051 | killagreg | 294 | AdNeutralNick = 0; |
295 | AdNeutralRoll = 0; |
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1 | ingob | 296 | AdNeutralGier = 0; |
1622 | killagreg | 297 | |
395 | hbuss | 298 | Parameter_AchsKopplung1 = 0; |
1120 | hbuss | 299 | Parameter_AchsKopplung2 = 0; |
1622 | killagreg | 300 | |
1036 | hbuss | 301 | ExpandBaro = 0; |
1622 | killagreg | 302 | |
1051 | killagreg | 303 | CalibrierMittelwert(); |
395 | hbuss | 304 | Delay_ms_Mess(100); |
1 | ingob | 305 | CalibrierMittelwert(); |
1622 | killagreg | 306 | |
1 | ingob | 307 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG)) // Höhenregelung aktiviert? |
1051 | killagreg | 308 | { |
2367 | holgerb | 309 | if((MessLuftdruck > 950) || (MessLuftdruck < 750) || ExpandBaro) SucheLuftruckOffset(); |
1 | ingob | 310 | } |
2367 | holgerb | 311 | |
312 | barotest = MessLuftdruck; |
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1166 | hbuss | 313 | #define NEUTRAL_FILTER 32 |
2367 | holgerb | 314 | OCR0A += OPA_OFFSET_STEP; |
315 | OCR0B = 255 - OCR0A; |
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1166 | hbuss | 316 | for(i=0; i<NEUTRAL_FILTER; i++) |
1111 | hbuss | 317 | { |
318 | Delay_ms_Mess(10); |
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1216 | killagreg | 319 | gier_neutral += AdWertGier; |
1166 | hbuss | 320 | nick_neutral += AdWertNick; |
321 | roll_neutral += AdWertRoll; |
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2316 | holgerb | 322 | acc_z_neutral += Aktuell_az; |
1111 | hbuss | 323 | } |
2367 | holgerb | 324 | if(MessLuftdruck < 1010 && MessLuftdruck > 20) BaroStep = barotest - MessLuftdruck; |
325 | OCR0A -= OPA_OFFSET_STEP; |
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326 | OCR0B = 255 - OCR0A; |
||
2316 | holgerb | 327 | AdNeutralNick = (nick_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER / 8); |
328 | AdNeutralRoll = (roll_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER / 8); |
||
329 | AdNeutralGier = (gier_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER); |
||
330 | NeutralAccZ = (acc_z_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER); |
||
1622 | killagreg | 331 | |
401 | hbuss | 332 | StartNeutralRoll = AdNeutralRoll; |
333 | StartNeutralNick = AdNeutralNick; |
||
1622 | killagreg | 334 | |
2319 | holgerb | 335 | if(AdjustmentMode == 2) |
1622 | killagreg | 336 | { |
337 | NeutralAccX = abs(Mittelwert_AccNick) / (2*ACC_AMPLIFY); |
||
338 | NeutralAccY = abs(Mittelwert_AccRoll) / (2*ACC_AMPLIFY); |
||
339 | // Save ACC neutral settings to eeprom |
||
1639 | holgerb | 340 | SetParamWord(PID_ACC_NICK, (uint16_t)NeutralAccX); |
341 | SetParamWord(PID_ACC_ROLL, (uint16_t)NeutralAccY); |
||
1622 | killagreg | 342 | SetParamWord(PID_ACC_TOP, (uint16_t)NeutralAccZ); |
513 | hbuss | 343 | } |
1051 | killagreg | 344 | else |
513 | hbuss | 345 | { |
1622 | killagreg | 346 | // restore from eeprom |
347 | NeutralAccX = (int16_t)GetParamWord(PID_ACC_NICK); |
||
348 | NeutralAccY = (int16_t)GetParamWord(PID_ACC_ROLL); |
||
349 | // strange settings? |
||
2316 | holgerb | 350 | if(((unsigned int) NeutralAccX > 2048) || ((unsigned int) NeutralAccY > 2048)/* || ((unsigned int) NeutralAccZ > 1024)*/) |
1622 | killagreg | 351 | { |
352 | printf("\n\rACC not calibrated!\r\n"); |
||
353 | NeutralAccX = abs(Mittelwert_AccNick) / (2*ACC_AMPLIFY); |
||
354 | NeutralAccY = abs(Mittelwert_AccRoll) / (2*ACC_AMPLIFY); |
||
2316 | holgerb | 355 | sucess = 0; |
1622 | killagreg | 356 | } |
513 | hbuss | 357 | } |
2330 | holgerb | 358 | EEAR = EE_DUMMY; // Set the EEPROM Address pointer to an unused space |
359 | MesswertNick = 0; |
||
1 | ingob | 360 | MesswertRoll = 0; |
361 | MesswertGier = 0; |
||
2367 | holgerb | 362 | Delay_ms_Mess(200); |
1703 | holgerb | 363 | Mittelwert_AccNick = ACC_AMPLIFY * AdWertAccNick; |
364 | Mittelwert_AccRoll = ACC_AMPLIFY * AdWertAccRoll; |
||
1173 | hbuss | 365 | IntegralNick = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccNick; |
366 | IntegralRoll = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccRoll; |
||
2072 | holgerb | 367 | Mess_IntegralNick = IntegralNick; |
368 | Mess_IntegralRoll = IntegralRoll; |
||
1173 | hbuss | 369 | Mess_Integral_Gier = 0; |
1837 | holgerb | 370 | KompassSollWert = KompassValue; |
1839 | holgerb | 371 | KompassSignalSchlecht = 100; |
882 | hbuss | 372 | Umschlag180Nick = ((long) EE_Parameter.WinkelUmschlagNick * 2500L) + 15000L; |
373 | Umschlag180Roll = ((long) EE_Parameter.WinkelUmschlagRoll * 2500L) + 15000L; |
||
492 | hbuss | 374 | ExternHoehenValue = 0; |
693 | hbuss | 375 | ErsatzKompass = KompassValue * GIER_GRAD_FAKTOR; |
376 | GierGyroFehler = 0; |
||
921 | hbuss | 377 | LED_Init(); |
2389 | holgerb | 378 | if(AdjustmentMode != 0) FC_StatusFlags |= FC_STATUS_CALIBRATE; |
992 | hbuss | 379 | FromNaviCtrl_Value.Kalman_K = -1; |
1173 | hbuss | 380 | FromNaviCtrl_Value.Kalman_MaxDrift = 0; |
992 | hbuss | 381 | FromNaviCtrl_Value.Kalman_MaxFusion = 32; |
1171 | hbuss | 382 | SenderOkay = 100; |
2349 | holgerb | 383 | |
384 | if(ServoActive) DDRD |=0x80; // enable J7 -> Servo signal |
||
385 | else |
||
1320 | hbuss | 386 | { |
2366 | holgerb | 387 | if((EE_Parameter.ServoCompInvert & SERVO_NICK_INV) && (EE_Parameter.ServoCompInvert & SERVO_RELATIVE)) NickServoValue = 12000;//((128 + 60) * 4 * 16); // neutral position = upper 1/4// else |
388 | else NickServoValue = ((128 - 60) * 4 * 16); // neutral position = lower 1/4 |
||
2349 | holgerb | 389 | CalculateServoSignals = 1; |
390 | CalculateServo(); // nick |
||
391 | CalculateServo(); // roll |
||
2240 | holgerb | 392 | } |
1702 | holgerb | 393 | |
2316 | holgerb | 394 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
395 | signed int tilt1, tilt2; |
||
396 | tilt1 = (int)(IntegralNick/GIER_GRAD_FAKTOR); // nick angle in deg |
||
397 | tilt2 = (int)(IntegralRoll/GIER_GRAD_FAKTOR); // roll angle in deg |
||
398 | tilt1 = (int16_t)ihypot(tilt1,tilt2); // tilt angle over all |
||
399 | CosAttitude = c_cos_8192(tilt1); |
||
400 | NeutralAccZ = (long)((long) (NeutralAccZ - 512) * 8192 + 4096) / CosAttitude + 512; |
||
401 | if(tilt1 > 20) sucess = 0; // calibration must be within 20° Tilt angle |
||
2427 | holgerb | 402 | if(AdjustmentMode != 0 && ACC_AltitudeControl) if((NeutralAccZ < 682 - 30) || (NeutralAccZ > 682 + 35)) { VersionInfo.HardwareError[0] |= FC_ERROR0_ACC_TOP; sucess = 0;}; |
2316 | holgerb | 403 | #else |
404 | NeutralAccZ = (int16_t)GetParamWord(PID_ACC_TOP); |
||
2330 | holgerb | 405 | EEAR = EE_DUMMY; // Set the EEPROM Address pointer to an unused space |
2316 | holgerb | 406 | #endif |
1765 | killagreg | 407 | if((AdNeutralNick < 150 * 16) || (AdNeutralNick > 850 * 16)) { VersionInfo.HardwareError[0] |= FC_ERROR0_GYRO_NICK; }; |
408 | if((AdNeutralRoll < 150 * 16) || (AdNeutralRoll > 850 * 16)) { VersionInfo.HardwareError[0] |= FC_ERROR0_GYRO_ROLL; }; |
||
409 | if((AdNeutralGier < 150 * 2) || (AdNeutralGier > 850 * 2)) { VersionInfo.HardwareError[0] |= FC_ERROR0_GYRO_YAW; }; |
||
410 | if((NeutralAccX < 300) || (NeutralAccX > 750)) { VersionInfo.HardwareError[0] |= FC_ERROR0_ACC_NICK; }; |
||
411 | if((NeutralAccY < 300) || (NeutralAccY > 750)) { VersionInfo.HardwareError[0] |= FC_ERROR0_ACC_ROLL; }; |
||
412 | if((NeutralAccZ < 512) || (NeutralAccZ > 850)) { VersionInfo.HardwareError[0] |= FC_ERROR0_ACC_TOP; }; |
||
2316 | holgerb | 413 | if(VersionInfo.HardwareError[0]) sucess = 0; |
1862 | holgerb | 414 | carefree_old = 70; |
1925 | holgerb | 415 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
1921 | holgerb | 416 | LIBFC_HoTT_Clear(); |
2316 | holgerb | 417 | ACC_AltitudeFusion(2); // initalisation |
1925 | holgerb | 418 | #endif |
2367 | holgerb | 419 | StartLuftdruck = Luftdruck; |
420 | VarioMeter = 0; |
||
421 | SummenHoehe = 0; Mess_Integral_Hoch = 0; |
||
2373 | holgerb | 422 | DebugOut.Analog[28] = 0; // I2C-Counter |
2367 | holgerb | 423 | CalcExpandBaroStep(); |
2316 | holgerb | 424 | return(sucess); |
1 | ingob | 425 | } |
426 | |||
1702 | holgerb | 427 | |
1 | ingob | 428 | //############################################################################ |
395 | hbuss | 429 | // Bearbeitet die Messwerte |
1 | ingob | 430 | void Mittelwert(void) |
431 | //############################################################################ |
||
1051 | killagreg | 432 | { |
1111 | hbuss | 433 | static signed long tmpl,tmpl2,tmpl3,tmpl4; |
434 | static signed int oldNick, oldRoll, d2Roll, d2Nick; |
||
1153 | hbuss | 435 | signed long winkel_nick, winkel_roll; |
1111 | hbuss | 436 | MesswertGier = (signed int) AdNeutralGier - AdWertGier; |
1171 | hbuss | 437 | MesswertNick = (signed int) AdWertNickFilter / 8; |
438 | MesswertRoll = (signed int) AdWertRollFilter / 8; |
||
1153 | hbuss | 439 | RohMesswertNick = MesswertNick; |
440 | RohMesswertRoll = MesswertRoll; |
||
1166 | hbuss | 441 | |
395 | hbuss | 442 | // Beschleunigungssensor ++++++++++++++++++++++++++++++++++++++++++++++++ |
1703 | holgerb | 443 | Mittelwert_AccNick = (Mittelwert_AccNick * 3 + ((ACC_AMPLIFY * AdWertAccNick))) / 4L; |
444 | Mittelwert_AccRoll = (Mittelwert_AccRoll * 3 + ((ACC_AMPLIFY * AdWertAccRoll))) / 4L; |
||
395 | hbuss | 445 | IntegralAccNick += ACC_AMPLIFY * AdWertAccNick; |
446 | IntegralAccRoll += ACC_AMPLIFY * AdWertAccRoll; |
||
805 | hbuss | 447 | NaviAccNick += AdWertAccNick; |
448 | NaviAccRoll += AdWertAccRoll; |
||
449 | NaviCntAcc++; |
||
1153 | hbuss | 450 | IntegralAccZ += Aktuell_az - NeutralAccZ; |
451 | |||
1155 | hbuss | 452 | //++++++++++++++++++++++++++++++++++++++++++++++++ |
2471 | holgerb | 453 | HoehenWert = HoehenWert_Mess; |
454 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
||
455 | HoehenWertF = HoehenWertF_Mess; |
||
456 | #else |
||
457 | HoehenWertF = HoehenWert; |
||
458 | #endif |
||
459 | //++++++++++++++++++++++++++++++++++++++++++++++++ |
||
1155 | hbuss | 460 | // ADC einschalten |
1171 | hbuss | 461 | ANALOG_ON; |
1155 | hbuss | 462 | AdReady = 0; |
463 | //++++++++++++++++++++++++++++++++++++++++++++++++ |
||
464 | |||
1216 | killagreg | 465 | if(Mess_IntegralRoll > 93000L) winkel_roll = 93000L; |
466 | else if(Mess_IntegralRoll <-93000L) winkel_roll = -93000L; |
||
1153 | hbuss | 467 | else winkel_roll = Mess_IntegralRoll; |
468 | |||
1216 | killagreg | 469 | if(Mess_IntegralNick > 93000L) winkel_nick = 93000L; |
470 | else if(Mess_IntegralNick <-93000L) winkel_nick = -93000L; |
||
1153 | hbuss | 471 | else winkel_nick = Mess_IntegralNick; |
472 | |||
1120 | hbuss | 473 | // Gier ++++++++++++++++++++++++++++++++++++++++++++++++ |
1153 | hbuss | 474 | Mess_Integral_Gier += MesswertGier; |
475 | ErsatzKompass += MesswertGier; |
||
395 | hbuss | 476 | // Kopplungsanteil +++++++++++++++++++++++++++++++++++++ |
1916 | holgerb | 477 | if(!Looping_Nick && !Looping_Roll && (Parameter_GlobalConfig & CFG_ACHSENKOPPLUNG_AKTIV)) |
395 | hbuss | 478 | { |
1153 | hbuss | 479 | tmpl3 = (MesswertRoll * winkel_nick) / 2048L; |
1120 | hbuss | 480 | tmpl3 *= Parameter_AchsKopplung2; //65 |
1111 | hbuss | 481 | tmpl3 /= 4096L; |
1153 | hbuss | 482 | tmpl4 = (MesswertNick * winkel_roll) / 2048L; |
1216 | killagreg | 483 | tmpl4 *= Parameter_AchsKopplung2; //65 |
1111 | hbuss | 484 | tmpl4 /= 4096L; |
1153 | hbuss | 485 | KopplungsteilNickRoll = tmpl3; |
486 | KopplungsteilRollNick = tmpl4; |
||
1111 | hbuss | 487 | tmpl4 -= tmpl3; |
488 | ErsatzKompass += tmpl4; |
||
1166 | hbuss | 489 | if(!Parameter_CouplingYawCorrection) Mess_Integral_Gier -= tmpl4/2; // Gier nachhelfen |
1111 | hbuss | 490 | |
1153 | hbuss | 491 | tmpl = ((MesswertGier + tmpl4) * winkel_nick) / 2048L; |
1111 | hbuss | 492 | tmpl *= Parameter_AchsKopplung1; // 90 |
880 | hbuss | 493 | tmpl /= 4096L; |
1153 | hbuss | 494 | tmpl2 = ((MesswertGier + tmpl4) * winkel_roll) / 2048L; |
395 | hbuss | 495 | tmpl2 *= Parameter_AchsKopplung1; |
1662 | killagreg | 496 | tmpl2 /= 4096L; |
1225 | hbuss | 497 | if(abs(MesswertGier) > 64) if(labs(tmpl) > 128 || labs(tmpl2) > 128) TrichterFlug = 1; |
1153 | hbuss | 498 | //MesswertGier += (Parameter_CouplingYawCorrection * tmpl4) / 256; |
395 | hbuss | 499 | } |
1166 | hbuss | 500 | else tmpl = tmpl2 = KopplungsteilNickRoll = KopplungsteilRollNick = 0; |
1658 | holgerb | 501 | TrimRoll = tmpl - tmpl2 / 100L; |
502 | TrimNick = -tmpl2 + tmpl / 100L; |
||
1111 | hbuss | 503 | // Kompasswert begrenzen ++++++++++++++++++++++++++++++++++++++++++++++++ |
504 | if(ErsatzKompass >= (360L * GIER_GRAD_FAKTOR)) ErsatzKompass -= 360L * GIER_GRAD_FAKTOR; // 360° Umschlag |
||
505 | if(ErsatzKompass < 0) ErsatzKompass += 360L * GIER_GRAD_FAKTOR; |
||
395 | hbuss | 506 | // Roll ++++++++++++++++++++++++++++++++++++++++++++++++ |
1166 | hbuss | 507 | Mess_IntegralRoll2 += MesswertRoll + TrimRoll; |
508 | Mess_IntegralRoll += MesswertRoll + TrimRoll - LageKorrekturRoll; |
||
1051 | killagreg | 509 | if(Mess_IntegralRoll > Umschlag180Roll) |
395 | hbuss | 510 | { |
882 | hbuss | 511 | Mess_IntegralRoll = -(Umschlag180Roll - 25000L); |
395 | hbuss | 512 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
1051 | killagreg | 513 | } |
395 | hbuss | 514 | if(Mess_IntegralRoll <-Umschlag180Roll) |
515 | { |
||
882 | hbuss | 516 | Mess_IntegralRoll = (Umschlag180Roll - 25000L); |
395 | hbuss | 517 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
1051 | killagreg | 518 | } |
395 | hbuss | 519 | // Nick ++++++++++++++++++++++++++++++++++++++++++++++++ |
1166 | hbuss | 520 | Mess_IntegralNick2 += MesswertNick + TrimNick; |
521 | Mess_IntegralNick += MesswertNick + TrimNick - LageKorrekturNick; |
||
1051 | killagreg | 522 | if(Mess_IntegralNick > Umschlag180Nick) |
882 | hbuss | 523 | { |
524 | Mess_IntegralNick = -(Umschlag180Nick - 25000L); |
||
525 | Mess_IntegralNick2 = Mess_IntegralNick; |
||
1051 | killagreg | 526 | } |
527 | if(Mess_IntegralNick <-Umschlag180Nick) |
||
395 | hbuss | 528 | { |
882 | hbuss | 529 | Mess_IntegralNick = (Umschlag180Nick - 25000L); |
395 | hbuss | 530 | Mess_IntegralNick2 = Mess_IntegralNick; |
1051 | killagreg | 531 | } |
1111 | hbuss | 532 | |
1 | ingob | 533 | Integral_Gier = Mess_Integral_Gier; |
534 | IntegralNick = Mess_IntegralNick; |
||
535 | IntegralRoll = Mess_IntegralRoll; |
||
1051 | killagreg | 536 | IntegralNick2 = Mess_IntegralNick2; |
1 | ingob | 537 | IntegralRoll2 = Mess_IntegralRoll2; |
538 | |||
1166 | hbuss | 539 | #define D_LIMIT 128 |
540 | |||
1171 | hbuss | 541 | MesswertNick = HiResNick / 8; |
542 | MesswertRoll = HiResRoll / 8; |
||
1166 | hbuss | 543 | |
1167 | hbuss | 544 | if(AdWertNick < 15) MesswertNick = -1000; if(AdWertNick < 7) MesswertNick = -2000; |
2426 | holgerb | 545 | // if(PlatinenVersion == 10) { if(AdWertNick > 1010) MesswertNick = +1000; if(AdWertNick > 1017) MesswertNick = +2000; } |
546 | // else |
||
547 | { if(AdWertNick > 2000) MesswertNick = +1000; if(AdWertNick > 2015) MesswertNick = +2000; } |
||
1167 | hbuss | 548 | if(AdWertRoll < 15) MesswertRoll = -1000; if(AdWertRoll < 7) MesswertRoll = -2000; |
2426 | holgerb | 549 | // if(PlatinenVersion == 10) { if(AdWertRoll > 1010) MesswertRoll = +1000; if(AdWertRoll > 1017) MesswertRoll = +2000; } |
550 | // else |
||
551 | { if(AdWertRoll > 2000) MesswertRoll = +1000; if(AdWertRoll > 2015) MesswertRoll = +2000; } |
||
1167 | hbuss | 552 | |
1216 | killagreg | 553 | if(Parameter_Gyro_D) |
1111 | hbuss | 554 | { |
1166 | hbuss | 555 | d2Nick = HiResNick - oldNick; |
556 | oldNick = (oldNick + HiResNick)/2; |
||
1111 | hbuss | 557 | if(d2Nick > D_LIMIT) d2Nick = D_LIMIT; |
558 | else if(d2Nick < -D_LIMIT) d2Nick = -D_LIMIT; |
||
1791 | holgerb | 559 | |
1166 | hbuss | 560 | d2Roll = HiResRoll - oldRoll; |
561 | oldRoll = (oldRoll + HiResRoll)/2; |
||
1111 | hbuss | 562 | if(d2Roll > D_LIMIT) d2Roll = D_LIMIT; |
563 | else if(d2Roll < -D_LIMIT) d2Roll = -D_LIMIT; |
||
1791 | holgerb | 564 | |
565 | MesswertNick += (d2Nick * (signed int) Parameter_Gyro_D) / 16; |
||
1166 | hbuss | 566 | MesswertRoll += (d2Roll * (signed int) Parameter_Gyro_D) / 16; |
567 | HiResNick += (d2Nick * (signed int) Parameter_Gyro_D); |
||
568 | HiResRoll += (d2Roll * (signed int) Parameter_Gyro_D); |
||
1216 | killagreg | 569 | } |
1111 | hbuss | 570 | |
1166 | hbuss | 571 | if(RohMesswertRoll > 0) TrimRoll += ((long) abs(KopplungsteilNickRoll) * Parameter_CouplingYawCorrection) / 64L; |
572 | else TrimRoll -= ((long) abs(KopplungsteilNickRoll) * Parameter_CouplingYawCorrection) / 64L; |
||
573 | if(RohMesswertNick > 0) TrimNick += ((long) abs(KopplungsteilRollNick) * Parameter_CouplingYawCorrection) / 64L; |
||
574 | else TrimNick -= ((long) abs(KopplungsteilRollNick) * Parameter_CouplingYawCorrection) / 64L; |
||
1153 | hbuss | 575 | |
1916 | holgerb | 576 | if(Parameter_GlobalConfig & CFG_DREHRATEN_BEGRENZER && !Looping_Nick && !Looping_Roll) |
1153 | hbuss | 577 | { |
578 | if(RohMesswertNick > 256) MesswertNick += 1 * (RohMesswertNick - 256); |
||
579 | else if(RohMesswertNick < -256) MesswertNick += 1 * (RohMesswertNick + 256); |
||
580 | if(RohMesswertRoll > 256) MesswertRoll += 1 * (RohMesswertRoll - 256); |
||
581 | else if(RohMesswertRoll < -256) MesswertRoll += 1 * (RohMesswertRoll + 256); |
||
582 | } |
||
1 | ingob | 583 | } |
584 | |||
585 | //############################################################################ |
||
586 | // Senden der Motorwerte per I2C-Bus |
||
587 | void SendMotorData(void) |
||
588 | //############################################################################ |
||
1051 | killagreg | 589 | { |
1209 | hbuss | 590 | unsigned char i; |
921 | hbuss | 591 | if(!MotorenEin) |
1 | ingob | 592 | { |
1765 | killagreg | 593 | FC_StatusFlags &= ~(FC_STATUS_MOTOR_RUN | FC_STATUS_FLY); |
2309 | holgerb | 594 | FC_StatusFlags2 &= ~FC_STATUS2_WAIT_FOR_TAKEOFF; |
1216 | killagreg | 595 | for(i=0;i<MAX_MOTORS;i++) |
596 | { |
||
597 | if(!PC_MotortestActive) MotorTest[i] = 0; |
||
1638 | holgerb | 598 | Motor[i].SetPoint = MotorTest[i]; |
599 | Motor[i].SetPointLowerBits = 0; |
||
600 | /* |
||
1760 | holgerb | 601 | Motor[i].SetPoint = MotorTest[i] / 4; // testing the high resolution |
602 | Motor[i].SetPointLowerBits = MotorTest[i] % 4; |
||
1638 | holgerb | 603 | */ |
1216 | killagreg | 604 | } |
1212 | hbuss | 605 | if(PC_MotortestActive) PC_MotortestActive--; |
1216 | killagreg | 606 | } |
1765 | killagreg | 607 | else FC_StatusFlags |= FC_STATUS_MOTOR_RUN; |
1744 | holgerb | 608 | |
2418 | holgerb | 609 | // ++++++++++++++++++++++++++++++++++++++++++ |
610 | |||
611 | // ++++++++++++++++++++++++++++++++++++++++++ |
||
2427 | holgerb | 612 | #ifdef REDUNDANT_FC_SLAVE |
2418 | holgerb | 613 | I2CTimeout = 100; |
614 | return; |
||
2427 | holgerb | 615 | #endif |
616 | |||
617 | #ifdef REDUNDANT_FC_MASTER |
||
618 | if(Parameter_UserParam7 > 150) |
||
2418 | holgerb | 619 | { |
2427 | holgerb | 620 | // Make noise |
621 | if((BeepMuster == 0xffff)) { beeptime = 25000; BeepMuster = 0x0080; } |
||
622 | // Do not send I2C-Data |
||
623 | if(RedundanceBlOperation) |
||
624 | { |
||
625 | I2CTimeout = 100; |
||
626 | return; |
||
627 | } |
||
2418 | holgerb | 628 | } |
629 | #endif |
||
630 | |||
1765 | killagreg | 631 | if(I2C_TransferActive) |
1744 | holgerb | 632 | { |
1760 | holgerb | 633 | I2C_TransferActive = 0; // enable for the next time |
1765 | killagreg | 634 | } |
635 | else |
||
1744 | holgerb | 636 | { |
2407 | holgerb | 637 | // motor_write = 0; |
1760 | holgerb | 638 | I2C_Start(TWI_STATE_MOTOR_TX); //Start I2C Interrupt Mode |
1765 | killagreg | 639 | } |
1 | ingob | 640 | } |
641 | |||
2342 | holgerb | 642 | unsigned char GetChannelValue(unsigned char ch) // gives the unsigned value of the channel |
643 | { |
||
644 | int tmp2; |
||
645 | if(ch == 0) return(0); |
||
646 | tmp2 = PPM_in[ch] + 127; |
||
647 | if(tmp2 > 255) tmp2 = 255; else if(tmp2 < 0) tmp2 = 0; |
||
648 | return(tmp2); |
||
649 | } |
||
1 | ingob | 650 | |
651 | //############################################################################ |
||
652 | // Trägt ggf. das Poti als Parameter ein |
||
1051 | killagreg | 653 | void ParameterZuordnung(void) |
1 | ingob | 654 | //############################################################################ |
655 | { |
||
1787 | holgerb | 656 | unsigned char tmp,i; |
657 | for(i=0;i<8;i++) |
||
658 | { |
||
659 | int tmp2; |
||
1933 | holgerb | 660 | tmp = EE_Parameter.Kanalbelegung[K_POTI1 + i]; |
661 | tmp2 = PPM_in[tmp] + 127; |
||
1787 | holgerb | 662 | if(tmp2 > 255) tmp2 = 255; else if(tmp2 < 0) tmp2 = 0; |
1933 | holgerb | 663 | |
664 | if(tmp == 25) Poti[i] = tmp2; // 25 = WaypointEvent channel -> no filter |
||
665 | else |
||
1787 | holgerb | 666 | if(tmp2 != Poti[i]) |
667 | { |
||
668 | Poti[i] += (tmp2 - Poti[i]) / 4; |
||
669 | if(Poti[i] > tmp2) Poti[i]--; |
||
670 | else Poti[i]++; |
||
671 | } |
||
672 | } |
||
921 | hbuss | 673 | CHK_POTI_MM(Parameter_Luftdruck_D,EE_Parameter.Luftdruck_D,0,100); |
674 | CHK_POTI_MM(Parameter_Hoehe_P,EE_Parameter.Hoehe_P,0,100); |
||
675 | CHK_POTI_MM(Parameter_Gyro_P,EE_Parameter.Gyro_P,10,255); |
||
1933 | holgerb | 676 | CHK_POTI_MM(Parameter_J16Timing,EE_Parameter.J16Timing,5,255); |
677 | CHK_POTI_MM(Parameter_J17Timing,EE_Parameter.J17Timing,5,255); |
||
2012 | holgerb | 678 | |
2443 | holgerb | 679 | if(EE_Parameter.Servo3 == 247) { if(PORTC & (1<<PORTC2)) Parameter_Servo3 = EE_Parameter.Servo3OnValue; else Parameter_Servo3 = EE_Parameter.Servo3OffValue;} // Out1 (J16) |
680 | else if(EE_Parameter.Servo3 == 246) { if(PORTC & (1<<PORTC3)) Parameter_Servo3 = EE_Parameter.Servo3OnValue; else Parameter_Servo3 = EE_Parameter.Servo3OffValue;} |
||
2349 | holgerb | 681 | else CHK_POTI_MM(Parameter_Servo3,EE_Parameter.Servo3, 24, 255); |
2012 | holgerb | 682 | |
2443 | holgerb | 683 | if(EE_Parameter.Servo4 == 247) { if(PORTC & (1<<PORTC2)) Parameter_Servo4 = EE_Parameter.Servo4OnValue; else Parameter_Servo4 = EE_Parameter.Servo4OffValue;} |
684 | else if(EE_Parameter.Servo4 == 246) { if(PORTC & (1<<PORTC3)) Parameter_Servo4 = EE_Parameter.Servo4OnValue; else Parameter_Servo4 = EE_Parameter.Servo4OffValue;} // Out2 (J17) |
||
2349 | holgerb | 685 | else CHK_POTI_MM(Parameter_Servo4,EE_Parameter.Servo4, 24, 255); |
686 | |||
687 | CHK_POTI_MM(Parameter_Servo5,EE_Parameter.Servo5, 24, 255); |
||
2342 | holgerb | 688 | Parameter_HoehenSchalter = GetChannelValue(EE_Parameter.HoeheChannel); |
1377 | hbuss | 689 | CHK_POTI(Parameter_Hoehe_ACC_Wirkung,EE_Parameter.Hoehe_ACC_Wirkung); |
690 | CHK_POTI(Parameter_Hoehe_GPS_Z,EE_Parameter.Hoehe_GPS_Z); |
||
691 | CHK_POTI(Parameter_KompassWirkung,EE_Parameter.KompassWirkung); |
||
692 | CHK_POTI(Parameter_Gyro_I,EE_Parameter.Gyro_I); |
||
693 | CHK_POTI(Parameter_Gyro_D,EE_Parameter.Gyro_D); |
||
694 | CHK_POTI(Parameter_Gyro_Gier_P,EE_Parameter.Gyro_Gier_P); |
||
695 | CHK_POTI(Parameter_Gyro_Gier_I,EE_Parameter.Gyro_Gier_I); |
||
696 | CHK_POTI(Parameter_I_Faktor,EE_Parameter.I_Faktor); |
||
697 | CHK_POTI(Parameter_UserParam1,EE_Parameter.UserParam1); |
||
698 | CHK_POTI(Parameter_UserParam2,EE_Parameter.UserParam2); |
||
699 | CHK_POTI(Parameter_UserParam3,EE_Parameter.UserParam3); |
||
700 | CHK_POTI(Parameter_UserParam4,EE_Parameter.UserParam4); |
||
701 | CHK_POTI(Parameter_UserParam5,EE_Parameter.UserParam5); |
||
702 | CHK_POTI(Parameter_UserParam6,EE_Parameter.UserParam6); |
||
703 | CHK_POTI(Parameter_UserParam7,EE_Parameter.UserParam7); |
||
704 | CHK_POTI(Parameter_UserParam8,EE_Parameter.UserParam8); |
||
705 | CHK_POTI(Parameter_ServoNickControl,EE_Parameter.ServoNickControl); |
||
706 | CHK_POTI(Parameter_ServoRollControl,EE_Parameter.ServoRollControl); |
||
2296 | holgerb | 707 | CHK_POTI(Parameter_ServoNickComp,EE_Parameter.ServoNickComp); |
708 | CHK_POTI(Parameter_ServoRollComp,EE_Parameter.ServoRollComp); |
||
1377 | hbuss | 709 | CHK_POTI(Parameter_LoopGasLimit,EE_Parameter.LoopGasLimit); |
1668 | holgerb | 710 | CHK_POTI(Parameter_AchsKopplung1,EE_Parameter.AchsKopplung1); |
711 | CHK_POTI(Parameter_AchsKopplung2,EE_Parameter.AchsKopplung2); |
||
1377 | hbuss | 712 | CHK_POTI(Parameter_CouplingYawCorrection,EE_Parameter.CouplingYawCorrection); |
1936 | holgerb | 713 | CHK_POTI(Parameter_MaximumAltitude,EE_Parameter.MaxAltitude); |
2447 | holgerb | 714 | // if((NC_To_FC_MaxAltitude && NC_To_FC_MaxAltitude < Parameter_MaximumAltitude) || Parameter_MaximumAltitude == 0) Parameter_MaximumAltitude = NC_To_FC_MaxAltitude; |
1916 | holgerb | 715 | Parameter_GlobalConfig = EE_Parameter.GlobalConfig; |
716 | Parameter_ExtraConfig = EE_Parameter.ExtraConfig; |
||
1377 | hbuss | 717 | // CHK_POTI(Parameter_AchsGegenKopplung1,EE_Parameter.AchsGegenKopplung1,0,255); |
718 | CHK_POTI(Parameter_DynamicStability,EE_Parameter.DynamicStability); |
||
719 | CHK_POTI(Parameter_ExternalControl,EE_Parameter.ExternalControl); |
||
1676 | holgerb | 720 | Ki = 10300 / (Parameter_I_Faktor + 1); |
1 | ingob | 721 | MAX_GAS = EE_Parameter.Gas_Max; |
1662 | killagreg | 722 | MIN_GAS = EE_Parameter.Gas_Min; |
1668 | holgerb | 723 | |
2342 | holgerb | 724 | if(EE_Parameter.CareFreeChannel) |
1668 | holgerb | 725 | { |
1682 | holgerb | 726 | CareFree = 1; |
2342 | holgerb | 727 | if(PPM_in[EE_Parameter.CareFreeChannel] < -64) CareFree = 0; |
728 | // if(tmp >= 248 && Poti[255 - tmp] < 50) CareFree = 0; |
||
1862 | holgerb | 729 | if(carefree_old != CareFree) |
730 | { |
||
731 | if(carefree_old < 3) |
||
732 | { |
||
2090 | holgerb | 733 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
734 | if(CareFree) { beeptime = 1500; if(!SpeakHoTT) SpeakHoTT = SPEAK_CF_ON; } |
||
735 | else { beeptime = 200; if(!SpeakHoTT) SpeakHoTT = SPEAK_CF_OFF; } |
||
736 | #else |
||
2063 | holgerb | 737 | if(CareFree) beeptime = 1500; |
1862 | holgerb | 738 | else beeptime = 200; |
2090 | holgerb | 739 | #endif |
2063 | holgerb | 740 | NeueKompassRichtungMerken = 5; |
1862 | holgerb | 741 | carefree_old = CareFree; |
742 | } else carefree_old--; |
||
743 | } |
||
1937 | holgerb | 744 | if(FromNaviCtrl.CompassValue < 0 && CareFree) VersionInfo.HardwareError[0] |= FC_ERROR0_CAREFREE; //else VersionInfo.HardwareError[0] &= ~FC_ERROR0_CAREFREE; |
1669 | killagreg | 745 | } |
1839 | holgerb | 746 | else |
747 | { |
||
748 | CareFree = 0; |
||
1862 | holgerb | 749 | carefree_old = 10; |
1839 | holgerb | 750 | } |
1668 | holgerb | 751 | |
1691 | holgerb | 752 | if(FromNaviCtrl.CompassValue < 0 && MotorenEin && CareFree && BeepMuster == 0xffff) // ungültiger Kompasswert |
1690 | holgerb | 753 | { |
754 | beeptime = 15000; |
||
755 | BeepMuster = 0xA400; |
||
756 | CareFree = 0; |
||
1765 | killagreg | 757 | } |
2341 | holgerb | 758 | if(CareFree) { FC_StatusFlags2 |= FC_STATUS2_CAREFREE; /*if(Parameter_AchsKopplung1 < 210) Parameter_AchsKopplung1 += 30;*/} else FC_StatusFlags2 &= ~FC_STATUS2_CAREFREE; |
1 | ingob | 759 | } |
760 | |||
2427 | holgerb | 761 | void CalcStickGasHover(void) |
762 | { |
||
763 | if(!EE_Parameter.Hoehe_StickNeutralPoint) |
||
764 | { |
||
765 | StickGasHover = HoverGas/STICK_GAIN; // rescale back to stick value |
||
766 | StickGasHover = (unsigned int)((unsigned int) StickGasHover * UBat) / BattLowVoltageWarning; |
||
767 | } |
||
768 | else StickGasHover = EE_Parameter.Hoehe_StickNeutralPoint; |
||
769 | LIMIT_MIN_MAX(StickGasHover, 70, 175); // reserve some range for trim up and down |
||
770 | } |
||
771 | |||
772 | |||
1 | ingob | 773 | //############################################################################ |
774 | // |
||
775 | void MotorRegler(void) |
||
776 | //############################################################################ |
||
777 | { |
||
1330 | killagreg | 778 | int pd_ergebnis_nick,pd_ergebnis_roll,tmp_int, tmp_int2; |
1 | ingob | 779 | int GierMischanteil,GasMischanteil; |
780 | static long sollGier = 0,tmp_long,tmp_long2; |
||
395 | hbuss | 781 | static long IntegralFehlerNick = 0; |
782 | static long IntegralFehlerRoll = 0; |
||
1 | ingob | 783 | static unsigned int RcLostTimer; |
784 | static unsigned char delay_neutral = 0; |
||
785 | static unsigned char delay_einschalten = 0,delay_ausschalten = 0; |
||
2146 | holgerb | 786 | static signed char move_safety_switch = 0; |
395 | hbuss | 787 | static long ausgleichNick, ausgleichRoll; |
1153 | hbuss | 788 | int IntegralNickMalFaktor,IntegralRollMalFaktor; |
1209 | hbuss | 789 | unsigned char i; |
1051 | killagreg | 790 | Mittelwert(); |
791 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
1 | ingob | 792 | // Gaswert ermitteln |
1051 | killagreg | 793 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
2230 | holgerb | 794 | if(!(FC_StatusFlags & (FC_STATUS_EMERGENCY_LANDING | FC_STATUS2_RC_FAILSAVE_ACTIVE))) |
795 | { |
||
796 | if(EE_Parameter.GlobalConfig3 & CFG3_VARIO_FAILSAFE) |
||
2028 | holgerb | 797 | { |
798 | if(HoverGas && HoverGas < 150 * STICK_GAIN) |
||
799 | { |
||
800 | HooverGasEmergencyPercent = (HoverGas/(STICK_GAIN) * EE_Parameter.NotGas) / 100; // i.e. 80% of Hovergas |
||
801 | } |
||
802 | else HooverGasEmergencyPercent = 45; // default if the Hoovergas was could not calculated yet |
||
803 | } else HooverGasEmergencyPercent = EE_Parameter.NotGas; |
||
2230 | holgerb | 804 | } |
805 | if(GasIsZeroCnt == 30000) // in that case we have RC-Lost, but the MK is probably landed |
||
806 | { |
||
807 | StickGas = 0; // Hold Gas down in that case |
||
808 | HooverGasEmergencyPercent = MIN_GAS; |
||
809 | } |
||
1051 | killagreg | 810 | GasMischanteil = StickGas; |
831 | hbuss | 811 | if(GasMischanteil < MIN_GAS + 10) GasMischanteil = MIN_GAS + 10; |
1051 | killagreg | 812 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
693 | hbuss | 813 | // Empfang schlecht |
1051 | killagreg | 814 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1916 | holgerb | 815 | if(SenderOkay < 100 && !(FC_StatusFlags2 & FC_STATUS2_RC_FAILSAVE_ACTIVE)) |
1 | ingob | 816 | { |
1051 | killagreg | 817 | if(RcLostTimer) RcLostTimer--; |
818 | else |
||
1 | ingob | 819 | { |
820 | MotorenEin = 0; |
||
1954 | holgerb | 821 | modell_fliegt = 0; |
822 | FC_StatusFlags &= ~(FC_STATUS_EMERGENCY_LANDING | FC_STATUS_FLY); |
||
1051 | killagreg | 823 | } |
1 | ingob | 824 | ROT_ON; |
2008 | holgerb | 825 | if(modell_fliegt > 1000 && Capacity.MinOfMaxPWM > 100) // wahrscheinlich in der Luft --> langsam absenken |
1 | ingob | 826 | { |
2028 | holgerb | 827 | GasMischanteil = HooverGasEmergencyPercent; |
1765 | killagreg | 828 | FC_StatusFlags |= FC_STATUS_EMERGENCY_LANDING; |
744 | hbuss | 829 | PPM_diff[EE_Parameter.Kanalbelegung[K_NICK]] = 0; |
1051 | killagreg | 830 | PPM_diff[EE_Parameter.Kanalbelegung[K_ROLL]] = 0; |
1 | ingob | 831 | PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] = 0; |
832 | PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] = 0; |
||
833 | PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] = 0; |
||
173 | holgerb | 834 | } |
1954 | holgerb | 835 | else |
836 | { |
||
837 | MotorenEin = 0; |
||
838 | } |
||
1 | ingob | 839 | } |
1051 | killagreg | 840 | else |
841 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
1 | ingob | 842 | // Emfang gut |
1051 | killagreg | 843 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 844 | if(SenderOkay > 140) |
845 | { |
||
2340 | holgerb | 846 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
2345 | holgerb | 847 | static unsigned int trigger = 1000; |
2340 | holgerb | 848 | static unsigned char old_switch = 100; |
849 | if(EE_Parameter.StartLandChannel && EE_Parameter.LandingSpeed) |
||
850 | { |
||
851 | if(PPM_in[EE_Parameter.StartLandChannel] > 50) |
||
852 | { |
||
853 | if(old_switch == 50) if(FC_StatusFlags2 & FC_STATUS2_WAIT_FOR_TAKEOFF) { FC_StatusFlags2 |= FC_STATUS2_AUTO_STARTING; SpeakHoTT = SPEAK_RISING;} |
||
2342 | holgerb | 854 | FC_StatusFlags2 &= ~FC_STATUS2_AUTO_LANDING; |
2340 | holgerb | 855 | old_switch = 150; |
856 | } |
||
857 | else |
||
858 | if(PPM_in[EE_Parameter.StartLandChannel] < -50) |
||
859 | { |
||
860 | if(old_switch == 150) { FC_StatusFlags2 |= FC_STATUS2_AUTO_LANDING; SpeakHoTT = SPEAK_SINKING;} |
||
2342 | holgerb | 861 | FC_StatusFlags2 &= ~FC_STATUS2_AUTO_STARTING; |
2340 | holgerb | 862 | old_switch = 50; |
863 | } |
||
864 | else |
||
865 | { |
||
866 | FC_StatusFlags2 &= ~(FC_STATUS2_AUTO_STARTING | FC_STATUS2_AUTO_LANDING); |
||
867 | } |
||
868 | } |
||
869 | #endif |
||
1765 | killagreg | 870 | FC_StatusFlags &= ~FC_STATUS_EMERGENCY_LANDING; |
1 | ingob | 871 | RcLostTimer = EE_Parameter.NotGasZeit * 50; |
921 | hbuss | 872 | if(GasMischanteil > 40 && MotorenEin) |
1 | ingob | 873 | { |
874 | if(modell_fliegt < 0xffff) modell_fliegt++; |
||
875 | } |
||
871 | hbuss | 876 | if((modell_fliegt < 256)) |
2309 | holgerb | 877 | { |
1 | ingob | 878 | SummeNick = 0; |
879 | SummeRoll = 0; |
||
1682 | holgerb | 880 | sollGier = 0; |
881 | Mess_Integral_Gier = 0; |
||
2309 | holgerb | 882 | FC_StatusFlags2 |= FC_STATUS2_WAIT_FOR_TAKEOFF; |
2340 | holgerb | 883 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
884 | old_switch = 100; |
||
885 | #endif |
||
2309 | holgerb | 886 | } |
887 | else |
||
888 | { |
||
889 | FC_StatusFlags |= FC_STATUS_FLY; |
||
890 | if(FC_StatusFlags2 & FC_STATUS2_WAIT_FOR_TAKEOFF) |
||
891 | { |
||
2322 | holgerb | 892 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
2340 | holgerb | 893 | if((NC_To_FC_Flags & NC_TO_FC_AUTOSTART || FC_StatusFlags2 & FC_STATUS2_AUTO_STARTING) && (VarioCharacter == '=') && ACC_AltitudeControl) |
2322 | holgerb | 894 | { |
2340 | holgerb | 895 | FromNC_AltitudeSpeed = 80; |
896 | FromNC_AltitudeSetpoint = 500; |
||
897 | SollHoehe = 500; |
||
2322 | holgerb | 898 | trigger = 1000; |
2340 | holgerb | 899 | if(NC_To_FC_Flags & NC_TO_FC_AUTOSTART) SpeakHoTT = SPEAK_NEXT_WP; |
2322 | holgerb | 900 | /* if(StartTrigger != 2) |
901 | { |
||
902 | StartTrigger = 1; |
||
903 | if(HoverGas < STICK_GAIN * 35) HoverGas = STICK_GAIN * 35; |
||
904 | } |
||
905 | */ |
||
906 | } |
||
2340 | holgerb | 907 | // else FC_StatusFlags2 &= ~(FC_STATUS2_AUTO_STARTING); |
2322 | holgerb | 908 | #endif |
2340 | holgerb | 909 | if(HoehenWertF > 150 || HoehenWert < -350 || !(Parameter_GlobalConfig & CFG_HOEHENREGELUNG)) |
2309 | holgerb | 910 | { |
911 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
||
2322 | holgerb | 912 | trigger = 1000; |
2369 | holgerb | 913 | if(FC_StatusFlags2 & FC_STATUS2_AUTO_STARTING) { FromNC_AltitudeSpeed = 0; SollHoehe = 300;/*HoehenWertF + 100;*/} |
914 | else SpeakHoTT = SPEAK_RISING; |
||
2309 | holgerb | 915 | #endif |
2340 | holgerb | 916 | FC_StatusFlags2 &= ~(FC_STATUS2_WAIT_FOR_TAKEOFF | FC_STATUS2_AUTO_STARTING | FC_STATUS2_AUTO_LANDING); |
2309 | holgerb | 917 | } |
918 | SummeNick = 0; |
||
919 | SummeRoll = 0; |
||
920 | Mess_Integral_Gier = 0; |
||
921 | // sollGier = 0; |
||
922 | if(modell_fliegt > 1000) modell_fliegt = 1000; // for the Hooverpoint-Estimation |
||
923 | } |
||
2322 | holgerb | 924 | else // Flying mode |
925 | { |
||
926 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
||
2340 | holgerb | 927 | if((FC_StatusFlags2 & FC_STATUS2_AUTO_LANDING) && (VarioCharacter == 'v' || VarioCharacter == '=') && ACC_AltitudeControl) |
928 | { |
||
929 | FromNC_AltitudeSpeed = EE_Parameter.LandingSpeed; |
||
930 | FromNC_AltitudeSetpoint = -20000; |
||
931 | } |
||
2322 | holgerb | 932 | if(trigger < 1000) |
933 | { |
||
934 | trigger++; |
||
935 | SummeNick = 0; |
||
936 | SummeRoll = 0; |
||
937 | Mess_Integral_Gier = 0; |
||
938 | SollHoehe = HoehenWertF - 300; |
||
2345 | holgerb | 939 | if(trigger == 1000 && FC_StatusFlags2 & FC_STATUS2_AUTO_LANDING && VarioCharacter != '+') |
940 | { |
||
941 | FC_StatusFlags2 &= ~FC_STATUS2_AUTO_LANDING; |
||
942 | FC_StatusFlags2 |= FC_STATUS2_WAIT_FOR_TAKEOFF; // go back into starting state |
||
943 | } |
||
2322 | holgerb | 944 | } |
945 | else |
||
946 | if(ACC_AltitudeControl && (VarioCharacter == 'v' || VarioCharacter == '-') && HoehenWert < 1000 /*&& FromNC_AltitudeSetpoint < 0*/) |
||
947 | { |
||
2345 | holgerb | 948 | if(Aktuell_az > 940) |
949 | { |
||
950 | trigger = 0; |
||
951 | SpeakHoTT = SPEAK_LANDING; |
||
952 | }; |
||
2322 | holgerb | 953 | } |
954 | #endif |
||
955 | } |
||
956 | } // end of: modell_fliegt > 256 |
||
595 | hbuss | 957 | if((PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] > 80) && MotorenEin == 0) |
1 | ingob | 958 | { |
1051 | killagreg | 959 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 960 | // auf Nullwerte kalibrieren |
1051 | killagreg | 961 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 962 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] > 75) // Neutralwerte |
963 | { |
||
964 | if(++delay_neutral > 200) // nicht sofort |
||
965 | { |
||
966 | delay_neutral = 0; |
||
967 | modell_fliegt = 0; |
||
968 | if(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70 || abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) > 70) |
||
969 | { |
||
304 | ingob | 970 | unsigned char setting=1; |
1 | ingob | 971 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < 70) setting = 1; |
972 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 2; |
||
973 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 3; |
||
974 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] <-70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 4; |
||
975 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] <-70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < 70) setting = 5; |
||
1622 | killagreg | 976 | SetActiveParamSet(setting); // aktiven Datensatz merken |
1 | ingob | 977 | } |
1051 | killagreg | 978 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) < 30 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < -70) |
979 | { |
||
819 | hbuss | 980 | WinkelOut.CalcState = 1; |
2009 | holgerb | 981 | CalibrationDone = 0; |
819 | hbuss | 982 | beeptime = 1000; |
983 | } |
||
984 | else |
||
1 | ingob | 985 | { |
2340 | holgerb | 986 | ParamSet_ReadFromEEProm(ActiveParamSet); |
1413 | killagreg | 987 | LipoDetection(0); |
1626 | killagreg | 988 | LIBFC_ReceiverInit(EE_Parameter.Receiver); |
1916 | holgerb | 989 | if((Parameter_GlobalConfig & CFG_HOEHENREGELUNG)) // Höhenregelung aktiviert? |
819 | hbuss | 990 | { |
1 | ingob | 991 | if((MessLuftdruck > 950) || (MessLuftdruck < 750)) SucheLuftruckOffset(); |
1051 | killagreg | 992 | } |
2319 | holgerb | 993 | CalibrationDone = SetNeutral(1); |
1232 | hbuss | 994 | ServoActive = 1; |
995 | DDRD |=0x80; // enable J7 -> Servo signal |
||
2263 | holgerb | 996 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
2309 | holgerb | 997 | if(VersionInfo.HardwareError[0]) SpeakHoTT = SPEAK_ERR_SENSOR; |
2316 | holgerb | 998 | else |
999 | if(!CalibrationDone) SpeakHoTT = SPEAK_ERR_CALIBARTION; |
||
2309 | holgerb | 1000 | else SpeakHoTT = SPEAK_CALIBRATE; |
2345 | holgerb | 1001 | ShowSettingNameTime = 5; // for HoTT & Jeti |
2263 | holgerb | 1002 | #endif |
2332 | holgerb | 1003 | Piep(ActiveParamSet,120); |
819 | hbuss | 1004 | } |
1051 | killagreg | 1005 | } |
1 | ingob | 1006 | } |
1051 | killagreg | 1007 | else |
513 | hbuss | 1008 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] < -75) // ACC Neutralwerte speichern |
1009 | { |
||
1010 | if(++delay_neutral > 200) // nicht sofort |
||
1011 | { |
||
1012 | MotorenEin = 0; |
||
1013 | delay_neutral = 0; |
||
1014 | modell_fliegt = 0; |
||
2319 | holgerb | 1015 | CalibrationDone = SetNeutral(2); // store ACC values into EEPROM |
2263 | holgerb | 1016 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
2316 | holgerb | 1017 | if(VersionInfo.HardwareError[0]) SpeakHoTT = SPEAK_ERR_SENSOR; |
1018 | else |
||
1019 | if(!CalibrationDone) SpeakHoTT = SPEAK_ERR_CALIBARTION; |
||
1020 | else SpeakHoTT = SPEAK_CALIBRATE; |
||
2263 | holgerb | 1021 | #endif |
2332 | holgerb | 1022 | Piep(ActiveParamSet,120); |
1051 | killagreg | 1023 | } |
513 | hbuss | 1024 | } |
1 | ingob | 1025 | else delay_neutral = 0; |
1026 | } |
||
1051 | killagreg | 1027 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 1028 | // Gas ist unten |
1051 | killagreg | 1029 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
2342 | holgerb | 1030 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] < -100) |
1 | ingob | 1031 | { |
2146 | holgerb | 1032 | if(PPM_diff[EE_Parameter.MotorSafetySwitch & 127] > 5) move_safety_switch = 100; |
1033 | else |
||
1034 | if(PPM_diff[EE_Parameter.MotorSafetySwitch & 127] < -5) move_safety_switch = -100; |
||
1521 | killagreg | 1035 | // Motoren Starten |
1036 | if(!MotorenEin) |
||
1037 | { |
||
2342 | holgerb | 1038 | if((((PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] < -100) && ((!(EE_Parameter.GlobalConfig3 & CFG3_MOTOR_SWITCH_MODE) && PPM_in[EE_Parameter.MotorSafetySwitch] < -75) || EE_Parameter.MotorSafetySwitch == 0))) |
2146 | holgerb | 1039 | || (((EE_Parameter.GlobalConfig3 & CFG3_MOTOR_SWITCH_MODE) && PPM_in[EE_Parameter.MotorSafetySwitch] > -10 && move_safety_switch == 100))) |
1521 | killagreg | 1040 | { |
1051 | killagreg | 1041 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 1042 | // Einschalten |
1051 | killagreg | 1043 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
2146 | holgerb | 1044 | if(CalibrationDone) FC_StatusFlags |= FC_STATUS_START; |
2367 | holgerb | 1045 | |
2309 | holgerb | 1046 | StartLuftdruck = Luftdruck; |
1047 | HoehenWert = 0; |
||
2471 | holgerb | 1048 | HoehenWert_Mess = 0; |
1049 | GasIsZeroCnt = 600; |
||
1050 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
||
1051 | HoehenWertF_Mess = 0; |
||
1052 | #endif |
||
2309 | holgerb | 1053 | SummenHoehe = 0; |
2367 | holgerb | 1054 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > -100 || abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) < 100) && EE_Parameter.MotorSafetySwitch == 0) delay_einschalten = 0; |
2146 | holgerb | 1055 | if(++delay_einschalten > 253) |
1521 | killagreg | 1056 | { |
2407 | holgerb | 1057 | if((abs(MesswertGier) > 32 || abs(MesswertNick) > 20) || abs(MesswertRoll) > 20) CalibrationDone = 0; // dann ist der Gyro defekt, schlecht kalibriert oder der MK dreht sich |
1521 | killagreg | 1058 | delay_einschalten = 0; |
2009 | holgerb | 1059 | if(!VersionInfo.HardwareError[0] && CalibrationDone && !NC_ErrorCode) |
1622 | killagreg | 1060 | { |
1061 | modell_fliegt = 1; |
||
1062 | MotorenEin = 1; |
||
1063 | sollGier = 0; |
||
1064 | Mess_Integral_Gier = 0; |
||
1065 | Mess_Integral_Gier2 = 0; |
||
1066 | Mess_IntegralNick = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccNick; |
||
1067 | Mess_IntegralRoll = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccRoll; |
||
1068 | Mess_IntegralNick2 = IntegralNick; |
||
1069 | Mess_IntegralRoll2 = IntegralRoll; |
||
1070 | SummeNick = 0; |
||
1071 | SummeRoll = 0; |
||
1913 | holgerb | 1072 | // ControlHeading = (((int) EE_Parameter.OrientationAngle * 15 + KompassValue) % 360) / 2; |
1840 | holgerb | 1073 | NeueKompassRichtungMerken = 100; // 2 sekunden |
2090 | holgerb | 1074 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
1075 | SpeakHoTT = SPEAK_STARTING; |
||
1076 | #endif |
||
1622 | killagreg | 1077 | } |
1078 | else |
||
1079 | { |
||
1080 | beeptime = 1500; // indicate missing calibration |
||
2090 | holgerb | 1081 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
2146 | holgerb | 1082 | if(!CalibrationDone) SpeakHoTT = SPEAK_ERR_CALIBARTION; |
2090 | holgerb | 1083 | #endif |
1622 | killagreg | 1084 | } |
1521 | killagreg | 1085 | } |
1086 | } |
||
1087 | else delay_einschalten = 0; |
||
1088 | } |
||
1051 | killagreg | 1089 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 1090 | // Auschalten |
1051 | killagreg | 1091 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1521 | killagreg | 1092 | else // only if motors are running |
1093 | { |
||
2146 | holgerb | 1094 | // if((PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] > 75) && (PPM_in[EE_Parameter.MotorSafetySwitch] < -75 || EE_Parameter.MotorSafetySwitch == 0)) |
2342 | holgerb | 1095 | if((((PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] > 100) && ((!(EE_Parameter.GlobalConfig3 & CFG3_MOTOR_SWITCH_MODE) && PPM_in[EE_Parameter.MotorSafetySwitch] < -75) || EE_Parameter.MotorSafetySwitch == 0))) |
2146 | holgerb | 1096 | || (((EE_Parameter.GlobalConfig3 & CFG3_MOTOR_SWITCH_MODE) && PPM_in[EE_Parameter.MotorSafetySwitch] < -50 && move_safety_switch == -100))) |
1521 | killagreg | 1097 | { |
2349 | holgerb | 1098 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > -100 || abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) < 100) && EE_Parameter.MotorSafetySwitch == 0) |
1099 | { |
||
1100 | delay_ausschalten = 0; |
||
1101 | } |
||
1102 | else |
||
1103 | { |
||
1104 | SummeNick = 0; |
||
1105 | SummeRoll = 0; |
||
1106 | StickNick = 0; |
||
1107 | StickRoll = 0; |
||
1108 | } |
||
2146 | holgerb | 1109 | if(++delay_ausschalten > 250) // nicht sofort |
1521 | killagreg | 1110 | { |
1111 | MotorenEin = 0; |
||
1112 | delay_ausschalten = 0; |
||
1113 | modell_fliegt = 0; |
||
2349 | holgerb | 1114 | FC_StatusFlags2 &= ~(FC_STATUS2_WAIT_FOR_TAKEOFF | FC_STATUS2_AUTO_STARTING | FC_STATUS2_AUTO_LANDING); |
1115 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
||
1116 | SpeakHoTT = SPEAK_MK_OFF; |
||
1117 | #endif |
||
1521 | killagreg | 1118 | } |
2366 | holgerb | 1119 | else |
1120 | if(delay_ausschalten == 100) beeptime = 3500; |
||
1521 | killagreg | 1121 | } |
1122 | else delay_ausschalten = 0; |
||
1123 | } |
||
2369 | holgerb | 1124 | if(GasIsZeroCnt < 1000) |
1125 | { |
||
1126 | if(VarioMeter > -150) GasIsZeroCnt++; |
||
1127 | else if(GasIsZeroCnt) GasIsZeroCnt--; |
||
1128 | } |
||
2230 | holgerb | 1129 | } |
2146 | holgerb | 1130 | else // gas not at minimum |
2230 | holgerb | 1131 | { |
1132 | move_safety_switch = 0; |
||
1133 | GasIsZeroCnt = 0; |
||
1134 | } |
||
1 | ingob | 1135 | } |
2230 | holgerb | 1136 | else // Empfang zwischen 100 und 140 -> schlecht |
1137 | { |
||
1138 | if(GasIsZeroCnt >= 750) // gas-stick was down for 1.5 seconds before RC-Lost |
||
1139 | { |
||
1140 | if((GPSInfo.HomeDistance < 40 * 10) && (HoehenWert < 15 * 100)) // and we are at the starting point -> maybe landed? |
||
1141 | { |
||
1142 | GasIsZeroCnt = 30000; |
||
1143 | if(modell_fliegt > 1001) modell_fliegt = 1001; |
||
1144 | } |
||
1145 | } |
||
1146 | } |
||
1051 | killagreg | 1147 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 1148 | // neue Werte von der Funke |
1051 | killagreg | 1149 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1216 | killagreg | 1150 | |
1765 | killagreg | 1151 | if(!NewPpmData-- || (FC_StatusFlags & FC_STATUS_EMERGENCY_LANDING)) |
1 | ingob | 1152 | { |
604 | hbuss | 1153 | static int stick_nick,stick_roll; |
1912 | holgerb | 1154 | unsigned char stick_p; |
1 | ingob | 1155 | ParameterZuordnung(); |
1912 | holgerb | 1156 | stick_p = EE_Parameter.Stick_P; |
1157 | stick_nick = (stick_nick * 3 + PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] * stick_p) / 4; |
||
723 | hbuss | 1158 | stick_nick += PPM_diff[EE_Parameter.Kanalbelegung[K_NICK]] * EE_Parameter.Stick_D; |
1912 | holgerb | 1159 | stick_roll = (stick_roll * 3 + PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] * stick_p) / 4; |
723 | hbuss | 1160 | stick_roll += PPM_diff[EE_Parameter.Kanalbelegung[K_ROLL]] * EE_Parameter.Stick_D; |
1161 | |||
1707 | holgerb | 1162 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1163 | // CareFree und freie Wahl der vorderen Richtung |
||
1164 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
1865 | holgerb | 1165 | if(CareFree) |
1166 | { |
||
1167 | signed int nick, roll; |
||
1168 | nick = stick_nick / 4; |
||
1169 | roll = stick_roll / 4; |
||
1170 | StickNick = ((FromNC_Rotate_C * nick) + (FromNC_Rotate_S * roll)) / (32 / 4); |
||
1171 | StickRoll = ((FromNC_Rotate_C * roll) - (FromNC_Rotate_S * nick)) / (32 / 4); |
||
1172 | } |
||
1173 | else |
||
1174 | { |
||
1175 | FromNC_Rotate_C = sintab[EE_Parameter.OrientationAngle + 6]; |
||
1176 | FromNC_Rotate_S = sintab[EE_Parameter.OrientationAngle]; |
||
1177 | StickNick = ((FromNC_Rotate_C * stick_nick) + (FromNC_Rotate_S * stick_roll)) / 8; |
||
1178 | StickRoll = ((FromNC_Rotate_C * stick_roll) - (FromNC_Rotate_S * stick_nick)) / 8; |
||
1179 | } |
||
1662 | killagreg | 1180 | |
1 | ingob | 1181 | StickGier = -PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]; |
1840 | holgerb | 1182 | if(StickGier > 4) StickGier -= 4; else |
1183 | if(StickGier < -4) StickGier += 4; else StickGier = 0; |
||
1120 | hbuss | 1184 | |
2369 | holgerb | 1185 | if(GasIsZeroCnt > 512) // About to switch - off |
1186 | { |
||
1187 | StickNick = StickNick/8; |
||
1188 | StickRoll = StickRoll/8; |
||
1189 | SummeNick = 0; |
||
1190 | SummeRoll = 0; |
||
1191 | } |
||
1192 | else |
||
1945 | holgerb | 1193 | if(GPS_Aid_StickMultiplikator) // in that case the GPS controls stronger |
1194 | { |
||
1195 | StickNick = (GPS_Aid_StickMultiplikator * (StickNick / 8)) / 16; |
||
1196 | StickRoll = (GPS_Aid_StickMultiplikator * (StickRoll / 8)) / 16; |
||
1197 | } |
||
1912 | holgerb | 1198 | StickNick -= GPS_Nick; |
1199 | StickRoll -= GPS_Roll; |
||
1933 | holgerb | 1200 | StickGas = PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] + 127; |
1330 | killagreg | 1201 | |
1153 | hbuss | 1202 | GyroFaktor = (Parameter_Gyro_P + 10.0); |
1203 | IntegralFaktor = Parameter_Gyro_I; |
||
1322 | hbuss | 1204 | GyroFaktorGier = (Parameter_Gyro_Gier_P + 10.0); |
1205 | IntegralFaktorGier = Parameter_Gyro_Gier_I; |
||
1 | ingob | 1206 | |
595 | hbuss | 1207 | //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1208 | //+ Analoge Steuerung per Seriell |
||
1209 | //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
921 | hbuss | 1210 | if(ExternControl.Config & 0x01 && Parameter_ExternalControl > 128) |
595 | hbuss | 1211 | { |
1212 | StickNick += (int) ExternControl.Nick * (int) EE_Parameter.Stick_P; |
||
1213 | StickRoll += (int) ExternControl.Roll * (int) EE_Parameter.Stick_P; |
||
1214 | StickGier += ExternControl.Gier; |
||
1215 | ExternHoehenValue = (int) ExternControl.Hight * (int)EE_Parameter.Hoehe_Verstaerkung; |
||
1216 | if(ExternControl.Gas < StickGas) StickGas = ExternControl.Gas; |
||
1217 | } |
||
855 | hbuss | 1218 | if(StickGas < 0) StickGas = 0; |
1330 | killagreg | 1219 | |
1916 | holgerb | 1220 | if(Parameter_GlobalConfig & CFG_HEADING_HOLD) IntegralFaktor = 0; |
723 | hbuss | 1221 | |
1051 | killagreg | 1222 | if(abs(StickNick/STICK_GAIN) > MaxStickNick) |
928 | hbuss | 1223 | { |
1051 | killagreg | 1224 | MaxStickNick = abs(StickNick)/STICK_GAIN; |
928 | hbuss | 1225 | if(MaxStickNick > 100) MaxStickNick = 100; |
1051 | killagreg | 1226 | } |
928 | hbuss | 1227 | else MaxStickNick--; |
1051 | killagreg | 1228 | if(abs(StickRoll/STICK_GAIN) > MaxStickRoll) |
928 | hbuss | 1229 | { |
1051 | killagreg | 1230 | MaxStickRoll = abs(StickRoll)/STICK_GAIN; |
928 | hbuss | 1231 | if(MaxStickRoll > 100) MaxStickRoll = 100; |
1051 | killagreg | 1232 | } |
928 | hbuss | 1233 | else MaxStickRoll--; |
1765 | killagreg | 1234 | if(FC_StatusFlags & FC_STATUS_EMERGENCY_LANDING) {MaxStickNick = 0; MaxStickRoll = 0;} |
723 | hbuss | 1235 | |
1051 | killagreg | 1236 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
173 | holgerb | 1237 | // Looping? |
1051 | killagreg | 1238 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
993 | hbuss | 1239 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_LINKS) Looping_Links = 1; |
1051 | killagreg | 1240 | else |
1241 | { |
||
395 | hbuss | 1242 | { |
1051 | killagreg | 1243 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < (EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese))) Looping_Links = 0; |
1244 | } |
||
1245 | } |
||
993 | hbuss | 1246 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < -EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_RECHTS) Looping_Rechts = 1; |
1051 | killagreg | 1247 | else |
395 | hbuss | 1248 | { |
1249 | if(Looping_Rechts) // Hysterese |
||
1250 | { |
||
1251 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > -(EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese)) Looping_Rechts = 0; |
||
1252 | } |
||
1051 | killagreg | 1253 | } |
173 | holgerb | 1254 | |
993 | hbuss | 1255 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_OBEN) Looping_Oben = 1; |
1051 | killagreg | 1256 | else |
1257 | { |
||
395 | hbuss | 1258 | if(Looping_Oben) // Hysterese |
1259 | { |
||
1051 | killagreg | 1260 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < (EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese))) Looping_Oben = 0; |
1261 | } |
||
1262 | } |
||
993 | hbuss | 1263 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < -EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_UNTEN) Looping_Unten = 1; |
1051 | killagreg | 1264 | else |
395 | hbuss | 1265 | { |
1266 | if(Looping_Unten) // Hysterese |
||
1267 | { |
||
1268 | if(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > -(EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese)) Looping_Unten = 0; |
||
1269 | } |
||
1051 | killagreg | 1270 | } |
395 | hbuss | 1271 | |
1272 | if(Looping_Links || Looping_Rechts) Looping_Roll = 1; else Looping_Roll = 0; |
||
1153 | hbuss | 1273 | if(Looping_Oben || Looping_Unten) { Looping_Nick = 1; Looping_Roll = 0; Looping_Links = 0; Looping_Rechts = 0;} else Looping_Nick = 0; |
395 | hbuss | 1274 | } // Ende neue Funken-Werte |
1275 | |||
1276 | if(Looping_Roll || Looping_Nick) |
||
1277 | { |
||
173 | holgerb | 1278 | if(GasMischanteil > EE_Parameter.LoopGasLimit) GasMischanteil = EE_Parameter.LoopGasLimit; |
1153 | hbuss | 1279 | TrichterFlug = 1; |
173 | holgerb | 1280 | } |
1281 | |||
1051 | killagreg | 1282 | |
1283 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
1284 | // Bei Empfangsausfall im Flug |
||
1285 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
1916 | holgerb | 1286 | if(FC_StatusFlags2 & FC_STATUS2_RC_FAILSAVE_ACTIVE) |
1287 | { |
||
1288 | StickNick = -GPS_Nick; |
||
1289 | StickRoll = -GPS_Roll; |
||
2230 | holgerb | 1290 | StickGas = StickGasHover; |
2407 | holgerb | 1291 | StickGier = 0; |
1916 | holgerb | 1292 | Parameter_GlobalConfig &= ~(CFG_HEADING_HOLD | CFG_DREHRATEN_BEGRENZER); |
1293 | Parameter_GlobalConfig |= CFG_HOEHENREGELUNG | CFG_ACHSENKOPPLUNG_AKTIV | CFG_KOMPASS_AKTIV | CFG_GPS_AKTIV | CFG_HOEHEN_SCHALTER | CFG_GPS_AKTIV; |
||
1294 | Parameter_ExtraConfig &= ~(CFG2_HEIGHT_LIMIT | CFG_LEARNABLE_CAREFREE | CFG2_VARIO_BEEP); |
||
1295 | Parameter_HoehenSchalter = 200; // switch on |
||
1296 | } |
||
1297 | else |
||
1765 | killagreg | 1298 | if(FC_StatusFlags & FC_STATUS_EMERGENCY_LANDING) |
1 | ingob | 1299 | { |
1300 | StickGier = 0; |
||
1301 | StickNick = 0; |
||
1302 | StickRoll = 0; |
||
1211 | hbuss | 1303 | GyroFaktor = 90; |
1304 | IntegralFaktor = 120; |
||
1305 | GyroFaktorGier = 90; |
||
1306 | IntegralFaktorGier = 120; |
||
173 | holgerb | 1307 | Looping_Roll = 0; |
1308 | Looping_Nick = 0; |
||
1051 | killagreg | 1309 | } |
395 | hbuss | 1310 | |
1051 | killagreg | 1311 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 1312 | // Integrale auf ACC-Signal abgleichen |
1051 | killagreg | 1313 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
395 | hbuss | 1314 | #define ABGLEICH_ANZAHL 256L |
1315 | |||
1316 | MittelIntegralNick += IntegralNick; // Für die Mittelwertbildung aufsummieren |
||
1317 | MittelIntegralRoll += IntegralRoll; |
||
1318 | MittelIntegralNick2 += IntegralNick2; |
||
1319 | MittelIntegralRoll2 += IntegralRoll2; |
||
1320 | |||
1321 | if(Looping_Nick || Looping_Roll) |
||
1322 | { |
||
1323 | IntegralAccNick = 0; |
||
1324 | IntegralAccRoll = 0; |
||
1325 | MittelIntegralNick = 0; |
||
1326 | MittelIntegralRoll = 0; |
||
1327 | MittelIntegralNick2 = 0; |
||
1328 | MittelIntegralRoll2 = 0; |
||
1329 | Mess_IntegralNick2 = Mess_IntegralNick; |
||
1330 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
||
1331 | ZaehlMessungen = 0; |
||
498 | hbuss | 1332 | LageKorrekturNick = 0; |
1333 | LageKorrekturRoll = 0; |
||
395 | hbuss | 1334 | } |
1335 | |||
1051 | killagreg | 1336 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1224 | hbuss | 1337 | if(!Looping_Nick && !Looping_Roll && (Aktuell_az > 512 || MotorenEin)) |
469 | hbuss | 1338 | { |
1339 | long tmp_long, tmp_long2; |
||
1839 | holgerb | 1340 | if(FromNaviCtrl_Value.Kalman_K > 0 /*&& !TrichterFlug*/) |
992 | hbuss | 1341 | { |
1944 | holgerb | 1342 | tmp_long = (long)(IntegralNick / EE_Parameter.GyroAccFaktor - (long)(Mittelwert_AccNick - FromNaviCtrl.AccErrorN)); |
1343 | tmp_long2 = (long)(IntegralRoll / EE_Parameter.GyroAccFaktor - (long)(Mittelwert_AccRoll - FromNaviCtrl.AccErrorR)); |
||
1344 | tmp_long = (tmp_long * FromNaviCtrl_Value.Kalman_K) / (32 * 16); |
||
1345 | tmp_long2 = (tmp_long2 * FromNaviCtrl_Value.Kalman_K) / (32 * 16); |
||
1346 | if((MaxStickNick > 64) || (MaxStickRoll > 64)) |
||
1347 | { |
||
1348 | tmp_long /= 2; |
||
1349 | tmp_long2 /= 2; |
||
1350 | } |
||
2309 | holgerb | 1351 | if(tmp_long > (long) FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long = (long) FromNaviCtrl_Value.Kalman_MaxFusion; |
1944 | holgerb | 1352 | if(tmp_long < (long)-FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long = (long)-FromNaviCtrl_Value.Kalman_MaxFusion; |
1353 | if(tmp_long2 > (long) FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long2 = (long) FromNaviCtrl_Value.Kalman_MaxFusion; |
||
1354 | if(tmp_long2 < (long)-FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long2 = (long)-FromNaviCtrl_Value.Kalman_MaxFusion; |
||
992 | hbuss | 1355 | } |
1051 | killagreg | 1356 | else |
992 | hbuss | 1357 | { |
1944 | holgerb | 1358 | tmp_long = (long)(IntegralNick / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccNick); |
1359 | tmp_long2 = (long)(IntegralRoll / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccRoll); |
||
1360 | tmp_long /= 16; |
||
1361 | tmp_long2 /= 16; |
||
1362 | if((MaxStickNick > 64) || (MaxStickRoll > 64)) |
||
1363 | { |
||
1364 | tmp_long /= 3; |
||
1365 | tmp_long2 /= 3; |
||
1366 | } |
||
1367 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25) |
||
1368 | { |
||
1369 | tmp_long /= 3; |
||
1370 | tmp_long2 /= 3; |
||
1371 | } |
||
1372 | KompassFusion = 25; |
||
1155 | hbuss | 1373 | #define AUSGLEICH 32 |
1944 | holgerb | 1374 | if(tmp_long > AUSGLEICH) tmp_long = AUSGLEICH; |
1375 | if(tmp_long < -AUSGLEICH) tmp_long =-AUSGLEICH; |
||
1376 | if(tmp_long2 > AUSGLEICH) tmp_long2 = AUSGLEICH; |
||
1377 | if(tmp_long2 <-AUSGLEICH) tmp_long2 =-AUSGLEICH; |
||
992 | hbuss | 1378 | } |
1166 | hbuss | 1379 | |
1111 | hbuss | 1380 | Mess_IntegralNick -= tmp_long; |
1381 | Mess_IntegralRoll -= tmp_long2; |
||
2437 | holgerb | 1382 | |
2439 | holgerb | 1383 | //DebugOut.Analog[16] += tmp_long; |
1384 | //DebugOut.Analog[17] += tmp_long2; |
||
2437 | holgerb | 1385 | |
469 | hbuss | 1386 | } |
1051 | killagreg | 1387 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
395 | hbuss | 1388 | if(ZaehlMessungen >= ABGLEICH_ANZAHL) |
1389 | { |
||
1390 | static int cnt = 0; |
||
1391 | static char last_n_p,last_n_n,last_r_p,last_r_n; |
||
1392 | static long MittelIntegralNick_Alt,MittelIntegralRoll_Alt; |
||
1173 | hbuss | 1393 | if(!Looping_Nick && !Looping_Roll && !TrichterFlug && EE_Parameter.Driftkomp) |
173 | holgerb | 1394 | { |
395 | hbuss | 1395 | MittelIntegralNick /= ABGLEICH_ANZAHL; |
1396 | MittelIntegralRoll /= ABGLEICH_ANZAHL; |
||
1397 | IntegralAccNick = (EE_Parameter.GyroAccFaktor * IntegralAccNick) / ABGLEICH_ANZAHL; |
||
1398 | IntegralAccRoll = (EE_Parameter.GyroAccFaktor * IntegralAccRoll) / ABGLEICH_ANZAHL; |
||
1399 | IntegralAccZ = IntegralAccZ / ABGLEICH_ANZAHL; |
||
1707 | holgerb | 1400 | #define MAX_I 0 |
395 | hbuss | 1401 | // Nick ++++++++++++++++++++++++++++++++++++++++++++++++ |
1402 | IntegralFehlerNick = (long)(MittelIntegralNick - (long)IntegralAccNick); |
||
1403 | ausgleichNick = IntegralFehlerNick / EE_Parameter.GyroAccAbgleich; |
||
1051 | killagreg | 1404 | // Roll ++++++++++++++++++++++++++++++++++++++++++++++++ |
1405 | IntegralFehlerRoll = (long)(MittelIntegralRoll - (long)IntegralAccRoll); |
||
395 | hbuss | 1406 | ausgleichRoll = IntegralFehlerRoll / EE_Parameter.GyroAccAbgleich; |
614 | hbuss | 1407 | |
1408 | LageKorrekturNick = ausgleichNick / ABGLEICH_ANZAHL; |
||
498 | hbuss | 1409 | LageKorrekturRoll = ausgleichRoll / ABGLEICH_ANZAHL; |
395 | hbuss | 1410 | |
992 | hbuss | 1411 | if(((MaxStickNick > 64) || (MaxStickRoll > 64) || (abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25)) && (FromNaviCtrl_Value.Kalman_K == -1)) |
614 | hbuss | 1412 | { |
1413 | LageKorrekturNick /= 2; |
||
720 | ingob | 1414 | LageKorrekturRoll /= 2; |
614 | hbuss | 1415 | } |
498 | hbuss | 1416 | |
1051 | killagreg | 1417 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
395 | hbuss | 1418 | // Gyro-Drift ermitteln |
1051 | killagreg | 1419 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
395 | hbuss | 1420 | MittelIntegralNick2 /= ABGLEICH_ANZAHL; |
1421 | MittelIntegralRoll2 /= ABGLEICH_ANZAHL; |
||
1051 | killagreg | 1422 | tmp_long = IntegralNick2 - IntegralNick; |
1423 | tmp_long2 = IntegralRoll2 - IntegralRoll; |
||
395 | hbuss | 1424 | |
1425 | IntegralFehlerNick = tmp_long; |
||
1426 | IntegralFehlerRoll = tmp_long2; |
||
1427 | Mess_IntegralNick2 -= IntegralFehlerNick; |
||
1428 | Mess_IntegralRoll2 -= IntegralFehlerRoll; |
||
1429 | |||
1111 | hbuss | 1430 | if(EE_Parameter.Driftkomp) |
1431 | { |
||
1622 | killagreg | 1432 | if(GierGyroFehler > ABGLEICH_ANZAHL/2) { AdNeutralGier++; } |
1433 | if(GierGyroFehler <-ABGLEICH_ANZAHL/2) { AdNeutralGier--; } |
||
1111 | hbuss | 1434 | } |
693 | hbuss | 1435 | GierGyroFehler = 0; |
720 | ingob | 1436 | |
1243 | killagreg | 1437 | #define FEHLER_LIMIT (ABGLEICH_ANZAHL / 2) |
1438 | #define FEHLER_LIMIT1 (ABGLEICH_ANZAHL * 2) //4 |
||
1225 | hbuss | 1439 | #define FEHLER_LIMIT2 (ABGLEICH_ANZAHL * 16) //16 |
492 | hbuss | 1440 | #define BEWEGUNGS_LIMIT 20000 |
395 | hbuss | 1441 | // Nick +++++++++++++++++++++++++++++++++++++++++++++++++ |
1442 | cnt = 1;// + labs(IntegralFehlerNick) / 4096; |
||
1225 | hbuss | 1443 | if(labs(IntegralFehlerNick) > FEHLER_LIMIT1) cnt = 4; |
1173 | hbuss | 1444 | if(labs(MittelIntegralNick_Alt - MittelIntegralNick) < BEWEGUNGS_LIMIT || (FromNaviCtrl_Value.Kalman_MaxDrift > 3*8)) |
492 | hbuss | 1445 | { |
1051 | killagreg | 1446 | if(IntegralFehlerNick > FEHLER_LIMIT2) |
395 | hbuss | 1447 | { |
1051 | killagreg | 1448 | if(last_n_p) |
395 | hbuss | 1449 | { |
1173 | hbuss | 1450 | cnt += labs(IntegralFehlerNick) / (FEHLER_LIMIT2 / 8); |
492 | hbuss | 1451 | ausgleichNick = IntegralFehlerNick / 8; |
401 | hbuss | 1452 | if(ausgleichNick > 5000) ausgleichNick = 5000; |
498 | hbuss | 1453 | LageKorrekturNick += ausgleichNick / ABGLEICH_ANZAHL; |
1051 | killagreg | 1454 | } |
395 | hbuss | 1455 | else last_n_p = 1; |
1456 | } else last_n_p = 0; |
||
1051 | killagreg | 1457 | if(IntegralFehlerNick < -FEHLER_LIMIT2) |
395 | hbuss | 1458 | { |
1459 | if(last_n_n) |
||
1051 | killagreg | 1460 | { |
1173 | hbuss | 1461 | cnt += labs(IntegralFehlerNick) / (FEHLER_LIMIT2 / 8); |
492 | hbuss | 1462 | ausgleichNick = IntegralFehlerNick / 8; |
401 | hbuss | 1463 | if(ausgleichNick < -5000) ausgleichNick = -5000; |
498 | hbuss | 1464 | LageKorrekturNick += ausgleichNick / ABGLEICH_ANZAHL; |
1051 | killagreg | 1465 | } |
395 | hbuss | 1466 | else last_n_n = 1; |
1467 | } else last_n_n = 0; |
||
1051 | killagreg | 1468 | } |
1469 | else |
||
847 | hbuss | 1470 | { |
1471 | cnt = 0; |
||
1839 | holgerb | 1472 | KompassSignalSchlecht = 100; |
1051 | killagreg | 1473 | } |
499 | hbuss | 1474 | if(cnt > EE_Parameter.Driftkomp) cnt = EE_Parameter.Driftkomp; |
1173 | hbuss | 1475 | if(FromNaviCtrl_Value.Kalman_MaxDrift) if(cnt > FromNaviCtrl_Value.Kalman_MaxDrift) cnt = FromNaviCtrl_Value.Kalman_MaxDrift; |
395 | hbuss | 1476 | if(IntegralFehlerNick > FEHLER_LIMIT) AdNeutralNick += cnt; |
1477 | if(IntegralFehlerNick < -FEHLER_LIMIT) AdNeutralNick -= cnt; |
||
401 | hbuss | 1478 | |
395 | hbuss | 1479 | // Roll +++++++++++++++++++++++++++++++++++++++++++++++++ |
1695 | holgerb | 1480 | cnt = 1;// + labs(IntegralFehlerRoll) / 4096; |
1225 | hbuss | 1481 | if(labs(IntegralFehlerRoll) > FEHLER_LIMIT1) cnt = 4; |
1173 | hbuss | 1482 | if(labs(MittelIntegralRoll_Alt - MittelIntegralRoll) < BEWEGUNGS_LIMIT || (FromNaviCtrl_Value.Kalman_MaxDrift > 3*8)) |
492 | hbuss | 1483 | { |
1051 | killagreg | 1484 | if(IntegralFehlerRoll > FEHLER_LIMIT2) |
395 | hbuss | 1485 | { |
1051 | killagreg | 1486 | if(last_r_p) |
395 | hbuss | 1487 | { |
1173 | hbuss | 1488 | cnt += labs(IntegralFehlerRoll) / (FEHLER_LIMIT2 / 8); |
492 | hbuss | 1489 | ausgleichRoll = IntegralFehlerRoll / 8; |
401 | hbuss | 1490 | if(ausgleichRoll > 5000) ausgleichRoll = 5000; |
498 | hbuss | 1491 | LageKorrekturRoll += ausgleichRoll / ABGLEICH_ANZAHL; |
1051 | killagreg | 1492 | } |
395 | hbuss | 1493 | else last_r_p = 1; |
1494 | } else last_r_p = 0; |
||
1051 | killagreg | 1495 | if(IntegralFehlerRoll < -FEHLER_LIMIT2) |
395 | hbuss | 1496 | { |
1051 | killagreg | 1497 | if(last_r_n) |
395 | hbuss | 1498 | { |
1173 | hbuss | 1499 | cnt += labs(IntegralFehlerRoll) / (FEHLER_LIMIT2 / 8); |
492 | hbuss | 1500 | ausgleichRoll = IntegralFehlerRoll / 8; |
401 | hbuss | 1501 | if(ausgleichRoll < -5000) ausgleichRoll = -5000; |
498 | hbuss | 1502 | LageKorrekturRoll += ausgleichRoll / ABGLEICH_ANZAHL; |
395 | hbuss | 1503 | } |
1504 | else last_r_n = 1; |
||
1505 | } else last_r_n = 0; |
||
1051 | killagreg | 1506 | } else |
492 | hbuss | 1507 | { |
1508 | cnt = 0; |
||
1839 | holgerb | 1509 | KompassSignalSchlecht = 100; |
1051 | killagreg | 1510 | } |
499 | hbuss | 1511 | if(cnt > EE_Parameter.Driftkomp) cnt = EE_Parameter.Driftkomp; |
1173 | hbuss | 1512 | if(FromNaviCtrl_Value.Kalman_MaxDrift) if(cnt > FromNaviCtrl_Value.Kalman_MaxDrift) cnt = FromNaviCtrl_Value.Kalman_MaxDrift; |
395 | hbuss | 1513 | if(IntegralFehlerRoll > FEHLER_LIMIT) AdNeutralRoll += cnt; |
1514 | if(IntegralFehlerRoll < -FEHLER_LIMIT) AdNeutralRoll -= cnt; |
||
173 | holgerb | 1515 | } |
1051 | killagreg | 1516 | else |
498 | hbuss | 1517 | { |
1518 | LageKorrekturRoll = 0; |
||
1519 | LageKorrekturNick = 0; |
||
880 | hbuss | 1520 | TrichterFlug = 0; |
498 | hbuss | 1521 | } |
1051 | killagreg | 1522 | |
498 | hbuss | 1523 | if(!IntegralFaktor) { LageKorrekturRoll = 0; LageKorrekturNick = 0;} // z.B. bei HH |
1051 | killagreg | 1524 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1525 | MittelIntegralNick_Alt = MittelIntegralNick; |
||
1526 | MittelIntegralRoll_Alt = MittelIntegralRoll; |
||
1527 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
395 | hbuss | 1528 | IntegralAccNick = 0; |
1529 | IntegralAccRoll = 0; |
||
1530 | IntegralAccZ = 0; |
||
1531 | MittelIntegralNick = 0; |
||
1532 | MittelIntegralRoll = 0; |
||
1533 | MittelIntegralNick2 = 0; |
||
1534 | MittelIntegralRoll2 = 0; |
||
1535 | ZaehlMessungen = 0; |
||
1173 | hbuss | 1536 | } // ZaehlMessungen >= ABGLEICH_ANZAHL |
395 | hbuss | 1537 | |
1051 | killagreg | 1538 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 1539 | // Gieren |
1051 | killagreg | 1540 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1840 | holgerb | 1541 | if(abs(StickGier) > 3) // war 15 |
1 | ingob | 1542 | { |
1839 | holgerb | 1543 | // KompassSignalSchlecht = 1000; |
1916 | holgerb | 1544 | if(!(Parameter_GlobalConfig & CFG_KOMPASS_FIX)) |
1051 | killagreg | 1545 | { |
1840 | holgerb | 1546 | NeueKompassRichtungMerken = 50; // eine Sekunde zum Einloggen |
824 | hbuss | 1547 | }; |
1 | ingob | 1548 | } |
1944 | holgerb | 1549 | tmp_int = (long) EE_Parameter.StickGier_P * ((long)StickGier * abs(StickGier)) / 512L; // expo y = ax + bx² |
1550 | tmp_int += (EE_Parameter.StickGier_P * StickGier) / 4; |
||
2309 | holgerb | 1551 | if(GasIsZeroCnt > 512) tmp_int = 0; // disable Yawing when Gas-Stick is to Zero |
1840 | holgerb | 1552 | tmp_int += CompassGierSetpoint; |
173 | holgerb | 1553 | sollGier = tmp_int; |
1051 | killagreg | 1554 | Mess_Integral_Gier -= tmp_int; |
395 | hbuss | 1555 | if(Mess_Integral_Gier > 50000) Mess_Integral_Gier = 50000; // begrenzen |
1556 | if(Mess_Integral_Gier <-50000) Mess_Integral_Gier =-50000; |
||
1051 | killagreg | 1557 | |
1558 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
1 | ingob | 1559 | // Kompass |
1051 | killagreg | 1560 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1916 | holgerb | 1561 | if(KompassValue >= 0 && (Parameter_GlobalConfig & CFG_KOMPASS_AKTIV)) |
1 | ingob | 1562 | { |
1839 | holgerb | 1563 | if(CalculateCompassTimer-- == 1) |
1564 | { |
||
1565 | int w,v,r,fehler,korrektur; // wird von der SPI-Routine auf 1 gesetzt |
||
1566 | CalculateCompassTimer = 13; // falls keine Navi-Daten |
||
1840 | holgerb | 1567 | // max. Korrekturwert schätzen |
1 | ingob | 1568 | w = abs(IntegralNick /512); // mit zunehmender Neigung den Einfluss drosseln |
1569 | v = abs(IntegralRoll /512); |
||
1570 | if(v > w) w = v; // grösste Neigung ermitteln |
||
1972 | holgerb | 1571 | // korrektur = w / 4 + 1; |
1572 | korrektur = w / 8 + 2; |
||
1941 | holgerb | 1573 | ErsatzKompassInGrad = ErsatzKompass/GIER_GRAD_FAKTOR; |
1840 | holgerb | 1574 | // Kompassfehlerwert bestimmen |
1941 | holgerb | 1575 | fehler = ((540 + KompassValue - ErsatzKompassInGrad) % 360) - 180; |
1840 | holgerb | 1576 | // GIER_GRAD_FAKTOR ist ca. 1200 |
1577 | // Kompasswert einloggen |
||
2439 | holgerb | 1578 | if(NeueKompassRichtungMerken) KompassSollWert = ErsatzKompassInGrad; |
1579 | |||
1840 | holgerb | 1580 | if(KompassSignalSchlecht) KompassSignalSchlecht--; |
1581 | else |
||
1582 | if(w < 25) |
||
921 | hbuss | 1583 | { |
1584 | GierGyroFehler += fehler; |
||
2439 | holgerb | 1585 | if(NeueKompassRichtungMerken) NeueKompassRichtungMerken--; |
1586 | /* if(NeueKompassRichtungMerken) |
||
1051 | killagreg | 1587 | { |
1839 | holgerb | 1588 | if(--NeueKompassRichtungMerken == 0) |
1589 | { |
||
1941 | holgerb | 1590 | KompassSollWert = ErsatzKompassInGrad; |
1839 | holgerb | 1591 | } |
921 | hbuss | 1592 | } |
2439 | holgerb | 1593 | */ |
1 | ingob | 1594 | } |
1840 | holgerb | 1595 | // Kompass fusionieren |
1839 | holgerb | 1596 | if(!KompassSignalSchlecht) ErsatzKompass += (fehler * KompassFusion) / korrektur; |
1941 | holgerb | 1597 | // MK Gieren |
1598 | if(!NeueKompassRichtungMerken) |
||
1839 | holgerb | 1599 | { |
1941 | holgerb | 1600 | r = ((540 + (KompassSollWert - ErsatzKompassInGrad)) % 360) - 180; |
1839 | holgerb | 1601 | v = r * (Parameter_KompassWirkung/2); // nach Kompass ausrichten |
1840 | holgerb | 1602 | CompassGierSetpoint = v / 16; |
1603 | } |
||
1865 | holgerb | 1604 | else CompassGierSetpoint = 0; |
1839 | holgerb | 1605 | } // CalculateCompassTimer |
1051 | killagreg | 1606 | } |
1840 | holgerb | 1607 | else CompassGierSetpoint = 0; |
1972 | holgerb | 1608 | |
1609 | //DebugOut.Analog[16] = KompassFusion; |
||
1051 | killagreg | 1610 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 1611 | // Drehgeschwindigkeit und -winkel zu einem Istwert zusammenfassen |
1051 | killagreg | 1612 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1216 | killagreg | 1613 | if(TrichterFlug) { SummeRoll = 0; SummeNick = 0;}; |
604 | hbuss | 1614 | |
1171 | hbuss | 1615 | if(!Looping_Nick) IntegralNickMalFaktor = (IntegralNick * IntegralFaktor) / (44000 / STICK_GAIN); else IntegralNickMalFaktor = 0; |
1616 | if(!Looping_Roll) IntegralRollMalFaktor = (IntegralRoll * IntegralFaktor) / (44000 / STICK_GAIN); else IntegralRollMalFaktor = 0; |
||
1153 | hbuss | 1617 | |
1167 | hbuss | 1618 | #define TRIM_MAX 200 |
1166 | hbuss | 1619 | if(TrimNick > TRIM_MAX) TrimNick = TRIM_MAX; else if(TrimNick <-TRIM_MAX) TrimNick =-TRIM_MAX; |
1620 | if(TrimRoll > TRIM_MAX) TrimRoll = TRIM_MAX; else if(TrimRoll <-TRIM_MAX) TrimRoll =-TRIM_MAX; |
||
1153 | hbuss | 1621 | |
1166 | hbuss | 1622 | MesswertNick = IntegralNickMalFaktor + (long)((long)MesswertNick * GyroFaktor + (long)TrimNick * 128L) / (256L / STICK_GAIN); |
1623 | MesswertRoll = IntegralRollMalFaktor + (long)((long)MesswertRoll * GyroFaktor + (long)TrimRoll * 128L) / (256L / STICK_GAIN); |
||
1211 | hbuss | 1624 | MesswertGier = (long)(MesswertGier * 2 * (long)GyroFaktorGier) / (256L / STICK_GAIN) + (long)(Integral_Gier * IntegralFaktorGier) / (2 * (44000 / STICK_GAIN)); |
1166 | hbuss | 1625 | |
1 | ingob | 1626 | // Maximalwerte abfangen |
1685 | holgerb | 1627 | #define MAX_SENSOR (4096) |
1216 | killagreg | 1628 | if(MesswertNick > MAX_SENSOR) MesswertNick = MAX_SENSOR; |
1 | ingob | 1629 | if(MesswertNick < -MAX_SENSOR) MesswertNick = -MAX_SENSOR; |
1630 | if(MesswertRoll > MAX_SENSOR) MesswertRoll = MAX_SENSOR; |
||
1631 | if(MesswertRoll < -MAX_SENSOR) MesswertRoll = -MAX_SENSOR; |
||
1632 | if(MesswertGier > MAX_SENSOR) MesswertGier = MAX_SENSOR; |
||
1633 | if(MesswertGier < -MAX_SENSOR) MesswertGier = -MAX_SENSOR; |
||
1634 | |||
1051 | killagreg | 1635 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
2390 | holgerb | 1636 | // Undervoltage |
1637 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
1638 | if(!(FC_StatusFlags & FC_STATUS_LOWBAT)) |
||
1639 | { |
||
1640 | GasMischanteil = ((unsigned int)GasMischanteil * BattLowVoltageWarning) / UBat; // Gas auf das aktuelle Spannungvieveau beziehen |
||
1641 | } |
||
1642 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
1643 | // Auto-Landing |
||
1644 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
1645 | static unsigned char slower; |
||
1646 | if(!slower--) |
||
1647 | { |
||
2402 | holgerb | 1648 | static unsigned int u_filter = 0; |
1649 | if(!u_filter) u_filter = UBat; |
||
1650 | if(UBat > u_filter) u_filter++; else |
||
1651 | if(UBat < u_filter) u_filter--; |
||
1652 | slower = 100; // 5Hz |
||
2416 | holgerb | 1653 | if(u_filter < BattAutoLandingVoltage) |
2390 | holgerb | 1654 | { |
2402 | holgerb | 1655 | LowVoltageLandingActive = 10; // 2 sek |
2390 | holgerb | 1656 | } |
2416 | holgerb | 1657 | else if(u_filter > BattAutoLandingVoltage + LipoCells && LowVoltageLandingActive) LowVoltageLandingActive--; |
2408 | holgerb | 1658 | |
2416 | holgerb | 1659 | if(u_filter < BattComingHomeVoltage) |
2408 | holgerb | 1660 | { |
1661 | LowVoltageHomeActive = 25; // min. 5 sek |
||
1662 | } |
||
2416 | holgerb | 1663 | else if(u_filter > BattComingHomeVoltage + LipoCells && LowVoltageHomeActive) LowVoltageHomeActive--; |
2390 | holgerb | 1664 | } |
1665 | if(LowVoltageLandingActive && FromNC_AltitudeSetpoint >= 0) |
||
1666 | { |
||
1667 | FromNC_AltitudeSpeed = EE_Parameter.LandingSpeed; |
||
1668 | FromNC_AltitudeSetpoint = -20000; |
||
1669 | } |
||
1670 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
2427 | holgerb | 1671 | // send SPI pending bytes |
1672 | if(BytegapSPI == 0) SPI_TransmitByte(); |
||
1673 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
1 | ingob | 1674 | // Höhenregelung |
1051 | killagreg | 1675 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
855 | hbuss | 1676 | GasMischanteil *= STICK_GAIN; |
2427 | holgerb | 1677 | // if height control is activated |
2334 | holgerb | 1678 | if((Parameter_GlobalConfig & CFG_HOEHENREGELUNG) && !(Looping_Roll || Looping_Nick) && !(VersionInfo.HardwareError[0] & 0x7F)) // Höhenregelung |
1309 | hbuss | 1679 | { |
1698 | holgerb | 1680 | #define HOVER_GAS_AVERAGE 16384L // 16384 * 2ms = 32s averaging |
1332 | hbuss | 1681 | #define HC_GAS_AVERAGE 4 // 4 * 2ms= 8ms averaging |
1638 | holgerb | 1682 | |
2309 | holgerb | 1683 | int HCGas, GasReduction = 0; |
1309 | hbuss | 1684 | static int HeightTrimming = 0; // rate for change of height setpoint |
2309 | holgerb | 1685 | static int HeightDeviation = 0, FilterHCGas = 0; |
1587 | killagreg | 1686 | static unsigned long HoverGasFilter = 0; |
1322 | hbuss | 1687 | static unsigned char delay = 100, BaroAtUpperLimit = 0, BaroAtLowerLimit = 0; |
1688 | // Expand the measurement |
||
1689 | // measurement of air pressure close to upper limit and no overflow in correction of the new OCR0A value occurs |
||
1690 | if(!BaroExpandActive) |
||
1691 | { |
||
1692 | if(MessLuftdruck > 920) |
||
1693 | { // increase offset |
||
1330 | killagreg | 1694 | if(OCR0A < (255 - OPA_OFFSET_STEP)) |
1322 | hbuss | 1695 | { |
1696 | ExpandBaro -= 1; |
||
1697 | OCR0A = DruckOffsetSetting - OPA_OFFSET_STEP * ExpandBaro; // increase offset to shift ADC down |
||
2367 | holgerb | 1698 | OCR0B = 255 - OCR0A; |
1322 | hbuss | 1699 | beeptime = 300; |
1352 | hbuss | 1700 | BaroExpandActive = 350; |
2367 | holgerb | 1701 | CalcExpandBaroStep(); |
1330 | killagreg | 1702 | } |
1703 | else |
||
1322 | hbuss | 1704 | { |
1705 | BaroAtLowerLimit = 1; |
||
1706 | } |
||
1707 | } |
||
1708 | // measurement of air pressure close to lower limit and |
||
1330 | killagreg | 1709 | else |
1322 | hbuss | 1710 | if(MessLuftdruck < 100) |
1711 | { // decrease offset |
||
1330 | killagreg | 1712 | if(OCR0A > OPA_OFFSET_STEP) |
1322 | hbuss | 1713 | { |
1714 | ExpandBaro += 1; |
||
1715 | OCR0A = DruckOffsetSetting - OPA_OFFSET_STEP * ExpandBaro; // decrease offset to shift ADC up |
||
2367 | holgerb | 1716 | OCR0B = 255 - OCR0A; |
1322 | hbuss | 1717 | beeptime = 300; |
1352 | hbuss | 1718 | BaroExpandActive = 350; |
2367 | holgerb | 1719 | CalcExpandBaroStep(); |
1330 | killagreg | 1720 | } |
1721 | else |
||
1322 | hbuss | 1722 | { |
1723 | BaroAtUpperLimit = 1; |
||
1724 | } |
||
1725 | } |
||
1330 | killagreg | 1726 | else |
1322 | hbuss | 1727 | { |
1728 | BaroAtUpperLimit = 0; |
||
1729 | BaroAtLowerLimit = 0; |
||
1730 | } |
||
1731 | } |
||
1732 | else // delay, because of expanding the Baro-Range |
||
1733 | { |
||
1734 | // now clear the D-values |
||
2316 | holgerb | 1735 | VarioMeter = 0; |
2309 | holgerb | 1736 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
2316 | holgerb | 1737 | if(ACC_AltitudeControl) ACC_AltitudeFusion(1); // init |
2309 | holgerb | 1738 | else SummenHoehe = HoehenWert * SM_FILTER; |
1739 | #else |
||
1740 | SummenHoehe = HoehenWert * SM_FILTER; |
||
1741 | #endif |
||
1322 | hbuss | 1742 | BaroExpandActive--; |
1743 | } |
||
1328 | hbuss | 1744 | // if height control is activated by an rc channel |
1916 | holgerb | 1745 | if(Parameter_GlobalConfig & CFG_HOEHEN_SCHALTER) // Regler wird über Schalter gesteuert |
1328 | hbuss | 1746 | { // check if parameter is less than activation threshold |
1916 | holgerb | 1747 | if(Parameter_HoehenSchalter < 50) // for 3 or 2-state switch height control is disabled in lowest position |
1328 | hbuss | 1748 | { //height control not active |
1749 | if(!delay--) |
||
1750 | { |
||
2090 | holgerb | 1751 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
2263 | holgerb | 1752 | if(!SpeakHoTT && HoehenReglerAktiv) SpeakHoTT = SPEAK_ALTITUDE_OFF; |
2090 | holgerb | 1753 | #endif |
1328 | hbuss | 1754 | HoehenReglerAktiv = 0; // disable height control |
1755 | SollHoehe = HoehenWert; // update SetPoint with current reading |
||
1756 | delay = 1; |
||
1757 | } |
||
1758 | } |
||
1759 | else |
||
2090 | holgerb | 1760 | if(Parameter_HoehenSchalter > 70) |
1328 | hbuss | 1761 | { //height control is activated |
2090 | holgerb | 1762 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
2263 | holgerb | 1763 | if(!SpeakHoTT && !HoehenReglerAktiv) SpeakHoTT = SPEAK_ALTITUDE_ON; |
2090 | holgerb | 1764 | #endif |
2263 | holgerb | 1765 | delay = 200; |
1328 | hbuss | 1766 | HoehenReglerAktiv = 1; // enable height control |
1767 | } |
||
1051 | killagreg | 1768 | } |
1309 | hbuss | 1769 | else // no switchable height control |
1770 | { |
||
1916 | holgerb | 1771 | SollHoehe = ((int16_t) ExternHoehenValue + (int16_t) Parameter_HoehenSchalter) * (int)EE_Parameter.Hoehe_Verstaerkung; |
1309 | hbuss | 1772 | HoehenReglerAktiv = 1; |
1051 | killagreg | 1773 | } |
1320 | hbuss | 1774 | // calculate cos of nick and roll angle used for projection of the vertical hoover gas |
1330 | killagreg | 1775 | tmp_int = (int)(IntegralNick/GIER_GRAD_FAKTOR); // nick angle in deg |
1776 | tmp_int2 = (int)(IntegralRoll/GIER_GRAD_FAKTOR); // roll angle in deg |
||
1777 | CosAttitude = (int16_t)ihypot(tmp_int, tmp_int2); // phytagoras gives effective attitude angle in deg |
||
1320 | hbuss | 1778 | LIMIT_MAX(CosAttitude, 60); // limit effective attitude angle |
1779 | CosAttitude = c_cos_8192(CosAttitude); // cos of actual attitude |
||
1591 | holgerb | 1780 | VarioCharacter = ' '; |
1942 | holgerb | 1781 | AltitudeSetpointTrimming = 0; |
1765 | killagreg | 1782 | if(HoehenReglerAktiv && !(FC_StatusFlags & FC_STATUS_EMERGENCY_LANDING)) |
1309 | hbuss | 1783 | { |
1784 | // Holger original version |
||
1785 | // start of height control algorithm |
||
1786 | // the height control is only an attenuation of the actual gas stick. |
||
1787 | // I.e. it will work only if the gas stick is higher than the hover gas |
||
1788 | // and the hover height will be allways larger than height setpoint. |
||
1861 | holgerb | 1789 | FC_StatusFlags2 |= FC_STATUS2_ALTITUDE_CONTROL; |
1916 | holgerb | 1790 | if((Parameter_ExtraConfig & CFG2_HEIGHT_LIMIT) || !(Parameter_GlobalConfig & CFG_HOEHEN_SCHALTER)) // Regler wird über Schalter gesteuert) |
1314 | killagreg | 1791 | { // old version |
1309 | hbuss | 1792 | HCGas = GasMischanteil; // take current stick gas as neutral point for the height control |
1793 | HeightTrimming = 0; |
||
1942 | holgerb | 1794 | AltitudeSetpointTrimming = 0; |
1773 | killagreg | 1795 | // set both flags to indicate no vario mode |
1796 | FC_StatusFlags |= (FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN); |
||
1309 | hbuss | 1797 | } |
1314 | killagreg | 1798 | else |
1309 | hbuss | 1799 | { |
1800 | // alternative height control |
||
1801 | // PD-Control with respect to hoover point |
||
1802 | // the thrust loss out of horizontal attitude is compensated |
||
1803 | // the setpoint will be fine adjusted with the gas stick position |
||
2390 | holgerb | 1804 | if(/*1 || */FC_StatusFlags & FC_STATUS_FLY) // trim setpoint only when flying |
1309 | hbuss | 1805 | { // gas stick is above hoover point |
1587 | killagreg | 1806 | if(StickGas > (StickGasHover + HEIGHT_CONTROL_STICKTHRESHOLD) && !BaroAtUpperLimit) |
1309 | hbuss | 1807 | { |
1767 | killagreg | 1808 | if(FC_StatusFlags & FC_STATUS_VARIO_TRIM_DOWN) |
1309 | hbuss | 1809 | { |
1767 | killagreg | 1810 | FC_StatusFlags &= ~FC_STATUS_VARIO_TRIM_DOWN; |
2309 | holgerb | 1811 | SollHoehe = HoehenWertF; // update setpoint to current heigth |
1309 | hbuss | 1812 | } |
1966 | holgerb | 1813 | // Limit the maximum Altitude |
2381 | holgerb | 1814 | if(Parameter_MaximumAltitude && (SollHoehe/100 > Parameter_MaximumAltitude)) |
1815 | { |
||
1816 | AltitudeSetpointTrimming = 0; |
||
1817 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
||
1818 | if(!SpeakHoTT && HoehenWert/95 > Parameter_MaximumAltitude) SpeakHoTT = SPEAK_MAX_ALTITUD; |
||
1819 | #endif |
||
1820 | VarioCharacter = '='; |
||
1821 | } |
||
1966 | holgerb | 1822 | else |
1823 | { |
||
2381 | holgerb | 1824 | if(HeightDeviation > 20) SollHoehe = HoehenWertF; // update setpoint to current heigth |
1825 | FC_StatusFlags |= FC_STATUS_VARIO_TRIM_UP; |
||
1942 | holgerb | 1826 | AltitudeSetpointTrimming = abs(StickGas - (StickGasHover + HEIGHT_CONTROL_STICKTHRESHOLD)); |
2390 | holgerb | 1827 | if(LowVoltageLandingActive) AltitudeSetpointTrimming /= 3; // only 33% rising |
1591 | holgerb | 1828 | VarioCharacter = '+'; |
1966 | holgerb | 1829 | } |
1865 | holgerb | 1830 | WaypointTrimming = 0; |
1309 | hbuss | 1831 | } // gas stick is below hoover point |
2390 | holgerb | 1832 | else if(StickGas < (StickGasHover - HEIGHT_CONTROL_STICKTHRESHOLD) && !BaroAtLowerLimit ) // Minus |
1309 | hbuss | 1833 | { |
2471 | holgerb | 1834 | if(FC_StatusFlags & FC_STATUS_VARIO_TRIM_UP || (HeightDeviation < -300)) |
1309 | hbuss | 1835 | { |
1767 | killagreg | 1836 | FC_StatusFlags &= ~FC_STATUS_VARIO_TRIM_UP; |
2309 | holgerb | 1837 | SollHoehe = HoehenWertF; // update setpoint to current heigth |
1309 | hbuss | 1838 | } |
1767 | killagreg | 1839 | FC_StatusFlags |= FC_STATUS_VARIO_TRIM_DOWN; |
1942 | holgerb | 1840 | AltitudeSetpointTrimming = -abs(StickGas - (StickGasHover - HEIGHT_CONTROL_STICKTHRESHOLD)); |
1591 | holgerb | 1841 | VarioCharacter = '-'; |
1865 | holgerb | 1842 | WaypointTrimming = 0; |
1309 | hbuss | 1843 | } |
1587 | killagreg | 1844 | else // Gas Stick in Hover Range |
1309 | hbuss | 1845 | { |
1855 | holgerb | 1846 | VarioCharacter = '='; |
1857 | holgerb | 1847 | if(FromNC_AltitudeSpeed && FromNC_AltitudeSetpoint > SollHoehe) // von NC gesteuert -> Steigen |
1855 | holgerb | 1848 | { |
1849 | FC_StatusFlags |= FC_STATUS_VARIO_TRIM_UP; |
||
1942 | holgerb | 1850 | AltitudeSetpointTrimming = FromNC_AltitudeSpeed; |
1851 | //HeightTrimming += FromNC_AltitudeSpeed; |
||
1857 | holgerb | 1852 | WaypointTrimming = 10; |
1853 | VarioCharacter = '^'; |
||
1865 | holgerb | 1854 | if(FC_StatusFlags & FC_STATUS_VARIO_TRIM_DOWN) // changed from sinking to rising |
1855 | { |
||
1856 | FC_StatusFlags &= ~FC_STATUS_VARIO_TRIM_DOWN; |
||
2309 | holgerb | 1857 | SollHoehe = HoehenWertF; // update setpoint to current heigth |
1865 | holgerb | 1858 | } |
1855 | holgerb | 1859 | } |
1860 | else |
||
1857 | holgerb | 1861 | if(FromNC_AltitudeSpeed && FromNC_AltitudeSetpoint < SollHoehe) // von NC gesteuert -> sinken |
1855 | holgerb | 1862 | { |
1863 | FC_StatusFlags |= FC_STATUS_VARIO_TRIM_DOWN; |
||
1942 | holgerb | 1864 | AltitudeSetpointTrimming = -FromNC_AltitudeSpeed; |
1865 | //HeightTrimming -= FromNC_AltitudeSpeed; |
||
1857 | holgerb | 1866 | WaypointTrimming = -10; |
1867 | VarioCharacter = 'v'; |
||
1865 | holgerb | 1868 | if(FC_StatusFlags & FC_STATUS_VARIO_TRIM_UP) // changed from rising to sinking |
1869 | { |
||
1870 | FC_StatusFlags &= ~FC_STATUS_VARIO_TRIM_UP; |
||
2309 | holgerb | 1871 | SollHoehe = HoehenWertF; // update setpoint to current heigth |
1865 | holgerb | 1872 | } |
1855 | holgerb | 1873 | } |
1874 | else |
||
1767 | killagreg | 1875 | if(FC_StatusFlags & (FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN)) |
1309 | hbuss | 1876 | { |
2309 | holgerb | 1877 | if(!WaypointTrimming) LIMIT_MIN_MAX(SollHoehe, (HoehenWertF-200), (HoehenWertF+200)) // max. 2m Unterschied |
1933 | holgerb | 1878 | else WaypointTrimming = 0; |
1767 | killagreg | 1879 | FC_StatusFlags &= ~(FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN); |
1309 | hbuss | 1880 | HeightTrimming = 0; |
1916 | holgerb | 1881 | if(Parameter_ExtraConfig & CFG2_VARIO_BEEP) beeptime = 500; |
1698 | holgerb | 1882 | if(!StartTrigger && HoehenWert > 50) |
1883 | { |
||
1884 | StartTrigger = 1; |
||
1765 | killagreg | 1885 | } |
1309 | hbuss | 1886 | } |
1887 | } |
||
1888 | // Trim height set point |
||
1942 | holgerb | 1889 | HeightTrimming += AltitudeSetpointTrimming; |
1890 | if(abs(HeightTrimming) > 500) // bei Waypoint-Flug ist das ca. die 500Hz |
||
1309 | hbuss | 1891 | { |
1857 | holgerb | 1892 | if(WaypointTrimming) |
1893 | { |
||
1894 | if(abs(FromNC_AltitudeSetpoint - SollHoehe) < 10) SollHoehe = FromNC_AltitudeSetpoint; |
||
1895 | else SollHoehe += WaypointTrimming; |
||
1896 | } |
||
1897 | else |
||
1966 | holgerb | 1898 | { |
1899 | if(HeightTrimming > 0) SollHoehe += EE_Parameter.Hoehe_Verstaerkung / 3; |
||
1900 | else SollHoehe -= EE_Parameter.Hoehe_Verstaerkung / 3; |
||
1901 | } |
||
1309 | hbuss | 1902 | HeightTrimming = 0; |
2471 | holgerb | 1903 | LIMIT_MIN_MAX(HoehenWertF, (HoehenWert-1024), (HoehenWert+1024)); // max. 10m Unterschied |
1904 | LIMIT_MIN_MAX(SollHoehe, (HoehenWertF-1024), (HoehenWertF+1024)); // max. 10m Unterschied |
||
1916 | holgerb | 1905 | if(Parameter_ExtraConfig & CFG2_VARIO_BEEP) beeptime = 100; |
1320 | hbuss | 1906 | //update hoover gas stick value when setpoint is shifted |
2427 | holgerb | 1907 | if(FromNC_AltitudeSpeed == 0) CalcStickGasHover(); |
1908 | /* |
||
1857 | holgerb | 1909 | if(!EE_Parameter.Hoehe_StickNeutralPoint && FromNC_AltitudeSpeed == 0) |
1332 | hbuss | 1910 | { |
1587 | killagreg | 1911 | StickGasHover = HoverGas/STICK_GAIN; //rescale back to stick value |
2427 | holgerb | 1912 | StickGasHover = (unsigned int)((unsigned int) StickGasHover * UBat) / BattLowVoltageWarning; |
1587 | killagreg | 1913 | if(StickGasHover < 70) StickGasHover = 70; |
2427 | holgerb | 1914 | else if(StickGasHover > 175) StickGasHover = 175; |
1332 | hbuss | 1915 | } |
2427 | holgerb | 1916 | */ |
1309 | hbuss | 1917 | } |
2309 | holgerb | 1918 | if(BaroExpandActive) SollHoehe = HoehenWertF; // update setpoint to current altitude if Expanding is active |
1420 | killagreg | 1919 | } //if FCFlags & MKFCFLAG_FLY |
1330 | killagreg | 1920 | else |
1921 | { |
||
2466 | holgerb | 1922 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
2462 | holgerb | 1923 | ACC_AltitudeFusion(1); // init the ACC and Altitude fusion |
2466 | holgerb | 1924 | #endif |
2471 | holgerb | 1925 | SollHoehe = HoehenWertF - 2000; |
1926 | |||
1587 | killagreg | 1927 | if(EE_Parameter.Hoehe_StickNeutralPoint) StickGasHover = EE_Parameter.Hoehe_StickNeutralPoint; |
2427 | holgerb | 1928 | else StickGasHover = 127; |
1698 | holgerb | 1929 | HoverGas = GasMischanteil; |
1972 | holgerb | 1930 | VarioCharacter = '.'; |
1320 | hbuss | 1931 | } |
1590 | killagreg | 1932 | HCGas = HoverGas; // take hover gas (neutral point) |
1933 | } |
||
2309 | holgerb | 1934 | if(HoehenWertF > SollHoehe || !(Parameter_ExtraConfig & CFG2_HEIGHT_LIMIT)) |
1283 | hbuss | 1935 | { |
2316 | holgerb | 1936 | if(!ACC_AltitudeControl) |
1937 | { |
||
1590 | killagreg | 1938 | // from this point the Heigth Control Algorithm is identical for both versions |
1939 | if(BaroExpandActive) // baro range expanding active |
||
1940 | { |
||
1941 | HCGas = HoverGas; // hover while expanding baro adc range |
||
1942 | HeightDeviation = 0; |
||
1943 | } // EOF // baro range expanding active |
||
1944 | else // valid data from air pressure sensor |
||
1945 | { |
||
1946 | // ------------------------- P-Part ---------------------------- |
||
2309 | holgerb | 1947 | tmp_long = (HoehenWertF - SollHoehe); // positive when too high |
1590 | killagreg | 1948 | LIMIT_MIN_MAX(tmp_long, -32767L, 32767L); // avoid overflov when casting to int16_t |
1949 | HeightDeviation = (int)(tmp_long); // positive when too high |
||
1695 | holgerb | 1950 | tmp_long = (tmp_long * (long)Parameter_Hoehe_P) / 32L; // p-part |
1698 | holgerb | 1951 | LIMIT_MIN_MAX(tmp_long, -127 * STICK_GAIN, 256 * STICK_GAIN); // more than the full range makes no sense |
1952 | GasReduction = tmp_long; |
||
1590 | killagreg | 1953 | // ------------------------- D-Part 1: Vario Meter ---------------------------- |
1954 | tmp_int = VarioMeter / 8; |
||
1765 | killagreg | 1955 | LIMIT_MIN_MAX(tmp_int, -127, 128); |
1705 | holgerb | 1956 | tmp_int = (tmp_int * (long)Parameter_Luftdruck_D) / 4L; // scale to d-gain parameter |
1957 | LIMIT_MIN_MAX(tmp_int,-64 * STICK_GAIN, 64 * STICK_GAIN); |
||
1767 | killagreg | 1958 | if(FC_StatusFlags & (FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN)) tmp_int /= 4; // reduce d-part while trimming setpoint |
1765 | killagreg | 1959 | else |
1916 | holgerb | 1960 | if(Parameter_ExtraConfig & CFG2_HEIGHT_LIMIT) tmp_int /= 8; // reduce d-part in "Deckel" mode |
1698 | holgerb | 1961 | GasReduction += tmp_int; |
1590 | killagreg | 1962 | } // EOF no baro range expanding |
1309 | hbuss | 1963 | // ------------------------ D-Part 2: ACC-Z Integral ------------------------ |
1698 | holgerb | 1964 | if(Parameter_Hoehe_ACC_Wirkung) |
1965 | { |
||
1966 | tmp_long = ((Mess_Integral_Hoch / 128L) * (int32_t) Parameter_Hoehe_ACC_Wirkung) / (128L / STICK_GAIN); |
||
1967 | LIMIT_MIN_MAX(tmp_long, -32 * STICK_GAIN, 64 * STICK_GAIN); |
||
1968 | GasReduction += tmp_long; |
||
1765 | killagreg | 1969 | } |
1587 | killagreg | 1970 | // ------------------------ D-Part 3: GpsZ ---------------------------------- |
1588 | killagreg | 1971 | tmp_int = (Parameter_Hoehe_GPS_Z * (int)FromNaviCtrl_Value.GpsZ)/128L; |
1972 | LIMIT_MIN_MAX(tmp_int, -32 * STICK_GAIN, 64 * STICK_GAIN); |
||
1698 | holgerb | 1973 | GasReduction += tmp_int; |
1701 | holgerb | 1974 | GasReduction = (long)((long)GasReduction * HoverGas) / 512; // scale to the gas value |
2309 | holgerb | 1975 | |
1701 | holgerb | 1976 | // ------------------------ ---------------------------------- |
1977 | HCGas -= GasReduction; |
||
1309 | hbuss | 1978 | // limit deviation from hoover point within the target region |
1942 | holgerb | 1979 | if(!AltitudeSetpointTrimming && HoverGas > 0) // height setpoint is not changed and hoover gas not zero |
1309 | hbuss | 1980 | { |
1765 | killagreg | 1981 | unsigned int tmp; |
1705 | holgerb | 1982 | tmp = abs(HeightDeviation); |
1983 | if(tmp <= 60) |
||
1984 | { |
||
1985 | LIMIT_MIN_MAX(HCGas, HoverGasMin, HoverGasMax); // limit gas around the hoover point |
||
1986 | } |
||
1987 | else |
||
1765 | killagreg | 1988 | { |
1705 | holgerb | 1989 | tmp = (tmp - 60) / 32; |
1692 | holgerb | 1990 | if(tmp > 15) tmp = 15; |
1705 | holgerb | 1991 | if(HeightDeviation > 0) |
1693 | holgerb | 1992 | { |
1705 | holgerb | 1993 | tmp = (HoverGasMin * (16 - tmp)) / 16; |
1994 | LIMIT_MIN_MAX(HCGas, tmp, HoverGasMax); // limit gas around the hoover point |
||
1693 | holgerb | 1995 | } |
1705 | holgerb | 1996 | else |
1997 | { |
||
1998 | tmp = (HoverGasMax * (tmp + 16)) / 16; |
||
1999 | LIMIT_MIN_MAX(HCGas, HoverGasMin, tmp); // limit gas around the hoover point |
||
2000 | } |
||
2001 | } |
||
1309 | hbuss | 2002 | } |
1322 | hbuss | 2003 | // strech control output by inverse attitude projection 1/cos |
2004 | // + 1/cos(angle) ++++++++++++++++++++++++++ |
||
1330 | killagreg | 2005 | tmp_long2 = (int32_t)HCGas; |
2006 | tmp_long2 *= 8192L; |
||
2007 | tmp_long2 /= CosAttitude; |
||
2008 | HCGas = (int16_t)tmp_long2; |
||
1309 | hbuss | 2009 | // update height control gas averaging |
2010 | FilterHCGas = (FilterHCGas * (HC_GAS_AVERAGE - 1) + HCGas) / HC_GAS_AVERAGE; |
||
2011 | // limit height control gas pd-control output |
||
2012 | LIMIT_MIN_MAX(FilterHCGas, EE_Parameter.Hoehe_MinGas * STICK_GAIN, (MAX_GAS - 20) * STICK_GAIN); |
||
2013 | // set GasMischanteil to HeightControlGasFilter |
||
1916 | holgerb | 2014 | if(Parameter_ExtraConfig & CFG2_HEIGHT_LIMIT) |
1587 | killagreg | 2015 | { // old version |
2016 | LIMIT_MAX(FilterHCGas, GasMischanteil); // nicht mehr als Gas |
||
1719 | holgerb | 2017 | GasMischanteil = FilterHCGas; |
1765 | killagreg | 2018 | } |
1719 | holgerb | 2019 | else GasMischanteil = FilterHCGas + (GasMischanteil - HoverGas) / 4; // only in Vario-Mode |
2316 | holgerb | 2020 | } |
2320 | holgerb | 2021 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
2316 | holgerb | 2022 | else // ACC-Altitude control |
2023 | { |
||
2309 | holgerb | 2024 | // from this point the Heigth Control Algorithm is identical for both versions |
2025 | if(BaroExpandActive) // baro range expanding active |
||
2026 | { |
||
2027 | HCGas = HoverGas; // hover while expanding baro adc range |
||
2028 | HeightDeviation = 0; |
||
2029 | } // EOF // baro range expanding active |
||
2030 | else // valid data from air pressure sensor |
||
2031 | { |
||
2032 | // ------------------------- P-Part ---------------------------- |
||
2033 | tmp_long = (HoehenWertF - SollHoehe); // positive when too high |
||
2034 | LIMIT_MIN_MAX(tmp_long, -32767L, 32767L); // avoid overflov when casting to int16_t |
||
2035 | HeightDeviation = (int)(tmp_long); // positive when too high |
||
2036 | tmp_long = (tmp_long * (long)Parameter_Hoehe_P) / 32L; // p-part |
||
2037 | LIMIT_MIN_MAX(tmp_long, -511 * STICK_GAIN, 512 * STICK_GAIN); // more than full range makes sense |
||
2038 | GasReduction = tmp_long; |
||
2039 | // ------------------------ D-Part: ACC-Z Integral ------------------------ |
||
2316 | holgerb | 2040 | tmp_long = VarioMeter + (AdWertAccHoch * Parameter_Hoehe_ACC_Wirkung)/256; |
2309 | holgerb | 2041 | // ------------------------- D-Part: Vario Meter ---------------------------- |
2042 | if(WaypointTrimming) { |
||
2043 | Variance = AltitudeSetpointTrimming * 8; |
||
2044 | } else { |
||
2045 | Variance = AltitudeSetpointTrimming * EE_Parameter.Hoehe_Verstaerkung*9/32; |
||
2046 | } |
||
2047 | tmp_long -= (long)Variance; |
||
2048 | tmp_long = (tmp_long * (long)Parameter_Luftdruck_D) / 32; // scale to d-gain parameter |
||
2049 | LIMIT_MIN_MAX(tmp_long,-511 * STICK_GAIN, 512 * STICK_GAIN); |
||
2050 | GasReduction += tmp_long; |
||
2051 | } // EOF no baro range expanding |
||
2052 | HCGas -= GasReduction; |
||
2053 | LIMIT_MIN_MAX(HCGas, HoverGasMin, HoverGasMax); // limits gas around hover point |
||
2054 | // strech control output by inverse attitude projection 1/cos |
||
2055 | // + 1/cos(angle) ++++++++++++++++++++++++++ |
||
2056 | tmp_long2 = (int32_t)HCGas; |
||
2057 | tmp_long2 *= 8192L; |
||
2058 | tmp_long2 /= CosAttitude; |
||
2059 | HCGas = (int16_t)tmp_long2; |
||
2060 | // update height control gas averaging |
||
2061 | FilterHCGas = (FilterHCGas * (HC_GAS_AVERAGE - 1) + HCGas) / HC_GAS_AVERAGE; |
||
2062 | // limit height control gas pd-control output |
||
2471 | holgerb | 2063 | int min; |
2064 | if(GasIsZeroCnt > 400 || (FC_StatusFlags2 & FC_STATUS2_WAIT_FOR_TAKEOFF)) min = EE_Parameter.Gas_Min; else min = EE_Parameter.Hoehe_MinGas; |
||
2065 | LIMIT_MIN_MAX(FilterHCGas, min * STICK_GAIN, (MAX_GAS - 20) * STICK_GAIN) |
||
2309 | holgerb | 2066 | // set GasMischanteil to HeightControlGasFilter |
2067 | if(Parameter_ExtraConfig & CFG2_HEIGHT_LIMIT) |
||
2068 | { // old version |
||
2069 | LIMIT_MAX(FilterHCGas, GasMischanteil); // nicht mehr als Gas |
||
2070 | GasMischanteil = FilterHCGas; |
||
2071 | } |
||
2316 | holgerb | 2072 | else GasMischanteil = FilterHCGas; |
2073 | } // end of ACC-Altitude control |
||
2320 | holgerb | 2074 | #endif |
1314 | killagreg | 2075 | } |
1309 | hbuss | 2076 | }// EOF height control active |
1320 | hbuss | 2077 | else // HC not active |
2078 | { |
||
2079 | //update hoover gas stick value when HC is not active |
||
2427 | holgerb | 2080 | CalcStickGasHover(); |
2081 | /* if(!EE_Parameter.Hoehe_StickNeutralPoint) |
||
1587 | killagreg | 2082 | { |
2083 | StickGasHover = HoverGas/STICK_GAIN; // rescale back to stick value |
||
2427 | holgerb | 2084 | StickGasHover = (unsigned int)((unsigned int) StickGasHover * UBat) / BattLowVoltageWarning; |
1322 | hbuss | 2085 | } |
1587 | killagreg | 2086 | else StickGasHover = EE_Parameter.Hoehe_StickNeutralPoint; |
2427 | holgerb | 2087 | LIMIT_MIN_MAX(StickGasHover, 70, 175); // reserve some range for trim up and down |
2088 | */ |
||
1328 | hbuss | 2089 | FilterHCGas = GasMischanteil; |
1773 | killagreg | 2090 | // set both flags to indicate no vario mode |
2091 | FC_StatusFlags |= (FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN); |
||
1861 | holgerb | 2092 | FC_StatusFlags2 &= ~FC_STATUS2_ALTITUDE_CONTROL; |
1330 | killagreg | 2093 | } |
1587 | killagreg | 2094 | // Hover gas estimation by averaging gas control output on small z-velocities |
1309 | hbuss | 2095 | // this is done only if height contol option is selected in global config and aircraft is flying |
1765 | killagreg | 2096 | if((FC_StatusFlags & FC_STATUS_FLY))// && !(FC_SatusFlags & FC_STATUS_EMERGENCY_LANDING)) |
1309 | hbuss | 2097 | { |
2316 | holgerb | 2098 | //if(HoverGasFilter == 0 || StartTrigger == 1) HoverGasFilter = HOVER_GAS_AVERAGE * (unsigned long)(GasMischanteil); // init estimation |
2318 | holgerb | 2099 | if(HoverGasFilter == 0 || StartTrigger == 1) HoverGasFilter = HOVER_GAS_AVERAGE * (unsigned long)(HoverGas); // 0.90f: geändert |
1698 | holgerb | 2100 | if(StartTrigger == 1) StartTrigger = 2; |
1330 | killagreg | 2101 | tmp_long2 = (int32_t)GasMischanteil; // take current thrust |
2102 | tmp_long2 *= CosAttitude; // apply attitude projection |
||
2103 | tmp_long2 /= 8192; |
||
1309 | hbuss | 2104 | // average vertical projected thrust |
1698 | holgerb | 2105 | if(modell_fliegt < 4000) // the first 8 seconds |
2106 | { // reduce the time constant of averaging by factor of 4 to get much faster a stable value |
||
2107 | HoverGasFilter -= HoverGasFilter/(HOVER_GAS_AVERAGE/16L); |
||
2108 | HoverGasFilter += 16L * tmp_long2; |
||
1309 | hbuss | 2109 | } |
1698 | holgerb | 2110 | if(modell_fliegt < 8000) // the first 16 seconds |
2111 | { // reduce the time constant of averaging by factor of 2 to get much faster a stable value |
||
1590 | killagreg | 2112 | HoverGasFilter -= HoverGasFilter/(HOVER_GAS_AVERAGE/4L); |
1587 | killagreg | 2113 | HoverGasFilter += 4L * tmp_long2; |
1309 | hbuss | 2114 | } |
1698 | holgerb | 2115 | else //later |
2316 | holgerb | 2116 | if(abs(VarioMeter) < 100 && abs(HoehenWertF - SollHoehe) < 256) // only on small vertical speed & difference is small (only descending) |
1309 | hbuss | 2117 | { |
1590 | killagreg | 2118 | HoverGasFilter -= HoverGasFilter/HOVER_GAS_AVERAGE; |
1587 | killagreg | 2119 | HoverGasFilter += tmp_long2; |
1309 | hbuss | 2120 | } |
1590 | killagreg | 2121 | HoverGas = (int16_t)(HoverGasFilter/HOVER_GAS_AVERAGE); |
1309 | hbuss | 2122 | if(EE_Parameter.Hoehe_HoverBand) |
2123 | { |
||
2124 | int16_t band; |
||
1587 | killagreg | 2125 | band = HoverGas / EE_Parameter.Hoehe_HoverBand; // the higher the parameter the smaller the range |
2126 | HoverGasMin = HoverGas - band; |
||
2127 | HoverGasMax = HoverGas + band; |
||
1309 | hbuss | 2128 | } |
2129 | else |
||
2130 | { // no limit |
||
1587 | killagreg | 2131 | HoverGasMin = 0; |
2132 | HoverGasMax = 1023; |
||
1309 | hbuss | 2133 | } |
1765 | killagreg | 2134 | } |
2135 | else |
||
1698 | holgerb | 2136 | { |
2137 | StartTrigger = 0; |
||
2138 | HoverGasFilter = 0; |
||
2139 | HoverGas = 0; |
||
1765 | killagreg | 2140 | } |
1916 | holgerb | 2141 | }// EOF Parameter_GlobalConfig & CFG_HEIGHT_CONTROL |
1773 | killagreg | 2142 | else |
2143 | { |
||
2144 | // set undefined state to indicate vario off |
||
2145 | FC_StatusFlags |= (FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN); |
||
2146 | } // EOF no height control |
||
2147 | |||
2309 | holgerb | 2148 | // Limits the maximum gas in case of "Out of Range emergency landing" |
2009 | holgerb | 2149 | if(NC_To_FC_Flags & NC_TO_FC_EMERGENCY_LANDING) |
2150 | { |
||
2028 | holgerb | 2151 | if(GasMischanteil/STICK_GAIN > HooverGasEmergencyPercent && HoverGas) GasMischanteil = HooverGasEmergencyPercent * STICK_GAIN; |
2309 | holgerb | 2152 | SollHoehe = HoehenWertF; // update setpoint to current heigth |
2009 | holgerb | 2153 | beeptime = 15000; |
2154 | BeepMuster = 0x0E00; |
||
2155 | } |
||
2028 | holgerb | 2156 | // limit gas to parameter setting |
1320 | hbuss | 2157 | LIMIT_MIN(GasMischanteil, (MIN_GAS + 10) * STICK_GAIN); |
855 | hbuss | 2158 | if(GasMischanteil > (MAX_GAS - 20) * STICK_GAIN) GasMischanteil = (MAX_GAS - 20) * STICK_GAIN; |
1111 | hbuss | 2159 | |
1051 | killagreg | 2160 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1320 | hbuss | 2161 | // all BL-Ctrl connected? |
2162 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
2418 | holgerb | 2163 | if(MissingMotor || Capacity.MinOfMaxPWM < 254 || NC_ErrorCode) // wait until all BL-Ctrls started and no Errors |
1931 | holgerb | 2164 | if(modell_fliegt > 1 && modell_fliegt < 50 && GasMischanteil > 0) // only during start-phase |
1320 | hbuss | 2165 | { |
2166 | modell_fliegt = 1; |
||
1675 | holgerb | 2167 | GasMischanteil = (MIN_GAS + 10) * STICK_GAIN; |
2382 | holgerb | 2168 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
2169 | if(Capacity.MinOfMaxPWM < 40) SpeakHoTT = SPEAK_ERR_MOTOR; |
||
2170 | #endif |
||
1320 | hbuss | 2171 | } |
2407 | holgerb | 2172 | |
2427 | holgerb | 2173 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
2174 | // send SPI pending bytes |
||
2407 | holgerb | 2175 | if(BytegapSPI == 0) SPI_TransmitByte(); |
1320 | hbuss | 2176 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 2177 | // + Mischer und PI-Regler |
1051 | killagreg | 2178 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
173 | holgerb | 2179 | DebugOut.Analog[7] = GasMischanteil; |
1051 | killagreg | 2180 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 2181 | // Gier-Anteil |
1051 | killagreg | 2182 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
855 | hbuss | 2183 | GierMischanteil = MesswertGier - sollGier * STICK_GAIN; // Regler für Gier |
2184 | #define MIN_GIERGAS (40*STICK_GAIN) // unter diesem Gaswert trotzdem Gieren |
||
693 | hbuss | 2185 | if(GasMischanteil > MIN_GIERGAS) |
2186 | { |
||
1051 | killagreg | 2187 | if(GierMischanteil > (GasMischanteil / 2)) GierMischanteil = GasMischanteil / 2; |
2188 | if(GierMischanteil < -(GasMischanteil / 2)) GierMischanteil = -(GasMischanteil / 2); |
||
693 | hbuss | 2189 | } |
1051 | killagreg | 2190 | else |
693 | hbuss | 2191 | { |
1051 | killagreg | 2192 | if(GierMischanteil > (MIN_GIERGAS / 2)) GierMischanteil = MIN_GIERGAS / 2; |
2193 | if(GierMischanteil < -(MIN_GIERGAS / 2)) GierMischanteil = -(MIN_GIERGAS / 2); |
||
693 | hbuss | 2194 | } |
855 | hbuss | 2195 | tmp_int = MAX_GAS*STICK_GAIN; |
1051 | killagreg | 2196 | if(GierMischanteil > ((tmp_int - GasMischanteil))) GierMischanteil = ((tmp_int - GasMischanteil)); |
855 | hbuss | 2197 | if(GierMischanteil < -((tmp_int - GasMischanteil))) GierMischanteil = -((tmp_int - GasMischanteil)); |
513 | hbuss | 2198 | |
1051 | killagreg | 2199 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 2200 | // Nick-Achse |
1051 | killagreg | 2201 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
723 | hbuss | 2202 | DiffNick = MesswertNick - StickNick; // Differenz bestimmen |
1153 | hbuss | 2203 | if(IntegralFaktor) SummeNick += IntegralNickMalFaktor - StickNick; // I-Anteil bei Winkelregelung |
1051 | killagreg | 2204 | else SummeNick += DiffNick; // I-Anteil bei HH |
855 | hbuss | 2205 | if(SummeNick > (STICK_GAIN * 16000L)) SummeNick = (STICK_GAIN * 16000L); |
2206 | if(SummeNick < -(16000L * STICK_GAIN)) SummeNick = -(16000L * STICK_GAIN); |
||
1791 | holgerb | 2207 | |
2208 | if(EE_Parameter.Gyro_Stability <= 8) pd_ergebnis_nick = (EE_Parameter.Gyro_Stability * DiffNick) / 8; // PI-Regler für Nick |
||
2209 | else pd_ergebnis_nick = ((EE_Parameter.Gyro_Stability / 2) * DiffNick) / 4; // Überlauf verhindern |
||
2210 | pd_ergebnis_nick += SummeNick / Ki; |
||
2211 | |||
1676 | holgerb | 2212 | tmp_int = (long)((long)Parameter_DynamicStability * (long)(GasMischanteil + abs(GierMischanteil)/2)) / 64; |
1153 | hbuss | 2213 | if(pd_ergebnis_nick > tmp_int) pd_ergebnis_nick = tmp_int; |
2214 | if(pd_ergebnis_nick < -tmp_int) pd_ergebnis_nick = -tmp_int; |
||
173 | holgerb | 2215 | |
1153 | hbuss | 2216 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
2217 | // Roll-Achse |
||
2218 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
2219 | DiffRoll = MesswertRoll - StickRoll; // Differenz bestimmen |
||
2220 | if(IntegralFaktor) SummeRoll += IntegralRollMalFaktor - StickRoll;// I-Anteil bei Winkelregelung |
||
2221 | else SummeRoll += DiffRoll; // I-Anteil bei HH |
||
2222 | if(SummeRoll > (STICK_GAIN * 16000L)) SummeRoll = (STICK_GAIN * 16000L); |
||
2223 | if(SummeRoll < -(16000L * STICK_GAIN)) SummeRoll = -(16000L * STICK_GAIN); |
||
1791 | holgerb | 2224 | |
2225 | if(EE_Parameter.Gyro_Stability <= 8) pd_ergebnis_roll = (EE_Parameter.Gyro_Stability * DiffRoll) / 8; // PI-Regler für Roll |
||
2226 | else pd_ergebnis_roll = ((EE_Parameter.Gyro_Stability / 2) * DiffRoll) / 4; // Überlauf verhindern |
||
2227 | pd_ergebnis_roll += SummeRoll / Ki; |
||
2228 | |||
1676 | holgerb | 2229 | tmp_int = (long)((long)Parameter_DynamicStability * (long)(GasMischanteil + abs(GierMischanteil)/2)) / 64; |
1153 | hbuss | 2230 | if(pd_ergebnis_roll > tmp_int) pd_ergebnis_roll = tmp_int; |
2231 | if(pd_ergebnis_roll < -tmp_int) pd_ergebnis_roll = -tmp_int; |
||
2232 | |||
2233 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
2427 | holgerb | 2234 | // send SPI pending bytes |
2235 | if(BytegapSPI == 0) SPI_TransmitByte(); |
||
2236 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
1209 | hbuss | 2237 | // Universal Mixer |
1155 | hbuss | 2238 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1642 | killagreg | 2239 | for(i=0; i<MAX_MOTORS; i++) |
2240 | { |
||
2241 | signed int tmp_int; |
||
2242 | if(Mixer.Motor[i][0] > 0) |
||
2243 | { |
||
1652 | holgerb | 2244 | // Gas |
1676 | holgerb | 2245 | if(Mixer.Motor[i][0] == 64) tmp_int = GasMischanteil; else tmp_int = ((long)GasMischanteil * Mixer.Motor[i][0]) / 64L; |
1652 | holgerb | 2246 | // Nick |
2247 | if(Mixer.Motor[i][1] == 64) tmp_int += pd_ergebnis_nick; |
||
2248 | else if(Mixer.Motor[i][1] == -64) tmp_int -= pd_ergebnis_nick; |
||
2249 | else tmp_int += ((long)pd_ergebnis_nick * Mixer.Motor[i][1]) / 64L; |
||
2250 | // Roll |
||
2251 | if(Mixer.Motor[i][2] == 64) tmp_int += pd_ergebnis_roll; |
||
2252 | else if(Mixer.Motor[i][2] == -64) tmp_int -= pd_ergebnis_roll; |
||
2253 | else tmp_int += ((long)pd_ergebnis_roll * Mixer.Motor[i][2]) / 64L; |
||
2254 | // Gier |
||
1676 | holgerb | 2255 | if(Mixer.Motor[i][3] == 64) tmp_int += GierMischanteil; |
2256 | else if(Mixer.Motor[i][3] == -64) tmp_int -= GierMischanteil; |
||
2257 | else tmp_int += ((long)GierMischanteil * Mixer.Motor[i][3]) / 64L; |
||
2427 | holgerb | 2258 | #ifdef REDUNDANT_FC_SLAVE |
2418 | holgerb | 2259 | tmp_int = (tmp_motorwert[i] + tmp_int) / 2; |
2260 | #else |
||
2386 | holgerb | 2261 | if(Motor[i].Version & MOTOR_STATE_FAST_MODE || tmp_int > tmp_motorwert[i]) tmp_int = (tmp_motorwert[i] + tmp_int) / 2; // Beschleunigen |
1913 | holgerb | 2262 | else |
2402 | holgerb | 2263 | { // BL-Ctrl 1.0 or 2.0 |
2386 | holgerb | 2264 | if(EE_Parameter.MotorSmooth == 0) |
1913 | holgerb | 2265 | { |
1931 | holgerb | 2266 | tmp_int = 2 * tmp_int - tmp_motorwert[i]; // original MotorSmoothing |
1913 | holgerb | 2267 | } |
2268 | else // 1 means tmp_int = tmp_int; |
||
2443 | holgerb | 2269 | if(EE_Parameter.MotorSmooth > 1) |
1913 | holgerb | 2270 | { |
2386 | holgerb | 2271 | // If >= 2 then allow >= 50% of the intended step down to rapidly reach the intended value. |
2272 | tmp_int = tmp_int + ((tmp_motorwert[i] - tmp_int) / EE_Parameter.MotorSmooth); |
||
1913 | holgerb | 2273 | } |
2274 | } |
||
2418 | holgerb | 2275 | #endif |
1760 | holgerb | 2276 | LIMIT_MIN_MAX(tmp_int,(int) MIN_GAS * 4,(int) MAX_GAS * 4); |
1676 | holgerb | 2277 | Motor[i].SetPoint = tmp_int / 4; |
1677 | killagreg | 2278 | Motor[i].SetPointLowerBits = (tmp_int % 4)<<1; // (3 bits total) |
1652 | holgerb | 2279 | tmp_motorwert[i] = tmp_int; |
1642 | killagreg | 2280 | } |
2281 | else |
||
2282 | { |
||
2283 | Motor[i].SetPoint = 0; |
||
2284 | Motor[i].SetPointLowerBits = 0; |
||
2285 | } |
||
2286 | } |
||
2427 | holgerb | 2287 | #ifdef REDUNDANT_FC_MASTER |
2437 | holgerb | 2288 | if(Parameter_UserParam6 > 230) Motor[0].SetPoint = 0; |
2427 | holgerb | 2289 | #endif |
2471 | holgerb | 2290 | |
1111 | hbuss | 2291 | } |
2090 | holgerb | 2292 | //DebugOut.Analog[16] |