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| Rev | Author | Line No. | Line |
|---|---|---|---|
| 1 | ingob | 1 | /*####################################################################################### |
| 2 | Flight Control |
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| 3 | #######################################################################################*/ |
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| 4 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
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| 1338 | ingob | 5 | // + Copyright (c) Holger Buss, Ingo Busker |
| 6 | // + Nur für den privaten Gebrauch / NON-COMMERCIAL USE ONLY |
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| 1 | ingob | 7 | // + www.MikroKopter.com |
| 8 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
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| 1051 | killagreg | 9 | // + Es gilt für das gesamte Projekt (Hardware, Software, Binärfiles, Sourcecode und Dokumentation), |
| 10 | // + dass eine Nutzung (auch auszugsweise) nur für den privaten (nicht-kommerziellen) Gebrauch zulässig ist. |
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| 11 | // + Sollten direkte oder indirekte kommerzielle Absichten verfolgt werden, ist mit uns (info@mikrokopter.de) Kontakt |
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| 12 | // + bzgl. der Nutzungsbedingungen aufzunehmen. |
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| 1 | ingob | 13 | // + Eine kommerzielle Nutzung ist z.B.Verkauf von MikroKoptern, Bestückung und Verkauf von Platinen oder Bausätzen, |
| 14 | // + Verkauf von Luftbildaufnahmen, usw. |
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| 15 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
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| 1051 | killagreg | 16 | // + Werden Teile des Quellcodes (mit oder ohne Modifikation) weiterverwendet oder veröffentlicht, |
| 1 | ingob | 17 | // + unterliegen sie auch diesen Nutzungsbedingungen und diese Nutzungsbedingungen incl. Copyright müssen dann beiliegen |
| 18 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
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| 19 | // + Sollte die Software (auch auszugesweise) oder sonstige Informationen des MikroKopter-Projekts |
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| 20 | // + auf anderen Webseiten oder sonstigen Medien veröffentlicht werden, muss unsere Webseite "http://www.mikrokopter.de" |
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| 21 | // + eindeutig als Ursprung verlinkt werden |
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| 22 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
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| 23 | // + Keine Gewähr auf Fehlerfreiheit, Vollständigkeit oder Funktion |
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| 24 | // + Benutzung auf eigene Gefahr |
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| 25 | // + Wir übernehmen keinerlei Haftung für direkte oder indirekte Personen- oder Sachschäden |
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| 26 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
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| 1338 | ingob | 27 | // + Die Portierung oder Nutzung der Software (oder Teile davon) auf andere Systeme (ausser der Hardware von www.mikrokopter.de) ist nur |
| 1 | ingob | 28 | // + mit unserer Zustimmung zulässig |
| 29 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
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| 30 | // + Die Funktion printf_P() unterliegt ihrer eigenen Lizenz und ist hiervon nicht betroffen |
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| 31 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
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| 1051 | killagreg | 32 | // + Redistributions of source code (with or without modifications) must retain the above copyright notice, |
| 1 | ingob | 33 | // + this list of conditions and the following disclaimer. |
| 34 | // + * Neither the name of the copyright holders nor the names of contributors may be used to endorse or promote products derived |
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| 35 | // + from this software without specific prior written permission. |
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| 1051 | killagreg | 36 | // + * The use of this project (hardware, software, binary files, sources and documentation) is only permittet |
| 1 | ingob | 37 | // + for non-commercial use (directly or indirectly) |
| 1051 | killagreg | 38 | // + Commercial use (for excample: selling of MikroKopters, selling of PCBs, assembly, ...) is only permitted |
| 1 | ingob | 39 | // + with our written permission |
| 1051 | killagreg | 40 | // + * If sources or documentations are redistributet on other webpages, out webpage (http://www.MikroKopter.de) must be |
| 41 | // + clearly linked as origin |
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| 1338 | ingob | 42 | // + * porting the sources to other systems or using the software on other systems (except hardware from www.mikrokopter.de) is not allowed |
| 1 | ingob | 43 | // + THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS "AS IS" |
| 44 | // + AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE |
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| 45 | // + IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE |
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| 46 | // + ARE DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT OWNER OR CONTRIBUTORS BE |
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| 47 | // + LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL, SPECIAL, EXEMPLARY, OR |
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| 48 | // + CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT LIMITED TO, PROCUREMENT OF |
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| 49 | // + SUBSTITUTE GOODS OR SERVICES; LOSS OF USE, DATA, OR PROFITS; OR BUSINESS |
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| 1322 | hbuss | 50 | // + INTERRUPTION) HOWEVER CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN |
| 51 | // + CONTRACT, STRICT LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) |
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| 1 | ingob | 52 | // + ARISING IN ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE |
| 1051 | killagreg | 53 | // + POSSIBILITY OF SUCH DAMAGE. |
| 1 | ingob | 54 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 55 | |||
| 56 | #include "main.h" |
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| 1320 | hbuss | 57 | #include "mymath.h" |
| 1330 | killagreg | 58 | #include "isqrt.h" |
| 1 | ingob | 59 | |
| 1352 | hbuss | 60 | unsigned char h,m,s; |
| 61 | unsigned int BaroExpandActive = 0; |
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| 173 | holgerb | 62 | volatile unsigned int I2CTimeout = 100; |
| 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; |
| 1643 | holgerb | 66 | int Mittelwert_AccNick, Mittelwert_AccRoll,Mittelwert_AccHoch; |
| 67 | unsigned int NeutralAccX=0, NeutralAccY=0; |
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| 805 | hbuss | 68 | int NaviAccNick, NaviAccRoll,NaviCntAcc = 0; |
| 1639 | holgerb | 69 | int NeutralAccZ = 0; |
| 1 | ingob | 70 | unsigned char CosinusNickWinkel = 0, CosinusRollWinkel = 0; |
| 693 | hbuss | 71 | long IntegralNick = 0,IntegralNick2 = 0; |
| 72 | long IntegralRoll = 0,IntegralRoll2 = 0; |
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| 73 | long IntegralAccNick = 0,IntegralAccRoll = 0,IntegralAccZ = 0; |
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| 74 | long Integral_Gier = 0; |
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| 75 | long Mess_IntegralNick = 0,Mess_IntegralNick2 = 0; |
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| 76 | long Mess_IntegralRoll = 0,Mess_IntegralRoll2 = 0; |
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| 77 | long Mess_Integral_Gier = 0,Mess_Integral_Gier2 = 0; |
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| 78 | long MittelIntegralNick,MittelIntegralRoll,MittelIntegralNick2,MittelIntegralRoll2; |
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| 1 | ingob | 79 | volatile long Mess_Integral_Hoch = 0; |
| 1153 | hbuss | 80 | int KompassValue = 0; |
| 81 | int KompassStartwert = 0; |
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| 82 | int KompassRichtung = 0; |
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| 693 | hbuss | 83 | unsigned int KompassSignalSchlecht = 500; |
| 855 | hbuss | 84 | unsigned char MAX_GAS,MIN_GAS; |
| 1 | ingob | 85 | unsigned char HoehenReglerAktiv = 0; |
| 880 | hbuss | 86 | unsigned char TrichterFlug = 0; |
| 395 | hbuss | 87 | long Umschlag180Nick = 250000L, Umschlag180Roll = 250000L; |
| 693 | hbuss | 88 | long ErsatzKompass; |
| 89 | int ErsatzKompassInGrad; // Kompasswert in Grad |
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| 90 | int GierGyroFehler = 0; |
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| 1211 | hbuss | 91 | char GyroFaktor,GyroFaktorGier; |
| 92 | char IntegralFaktor,IntegralFaktorGier; |
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| 1153 | hbuss | 93 | int DiffNick,DiffRoll; |
| 1377 | hbuss | 94 | //int Poti1 = 0, Poti2 = 0, Poti3 = 0, Poti4 = 0, Poti5 = 0, Poti6 = 0, Poti7 = 0, Poti8 = 0; |
| 1391 | killagreg | 95 | unsigned char Poti[9] = {0,0,0,0,0,0,0,0}; |
| 1 | ingob | 96 | volatile unsigned char SenderOkay = 0; |
| 595 | hbuss | 97 | int StickNick = 0,StickRoll = 0,StickGier = 0,StickGas = 0; |
| 1 | ingob | 98 | char MotorenEin = 0; |
| 1622 | killagreg | 99 | unsigned char RequiredMotors = 0; |
| 1246 | killagreg | 100 | long HoehenWert = 0; |
| 101 | long SollHoehe = 0; |
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| 498 | hbuss | 102 | int LageKorrekturRoll = 0,LageKorrekturNick = 0; |
| 1153 | hbuss | 103 | //float Ki = FAKTOR_I; |
| 104 | int Ki = 10300 / 33; |
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| 395 | hbuss | 105 | unsigned char Looping_Nick = 0,Looping_Roll = 0; |
| 106 | unsigned char Looping_Links = 0, Looping_Rechts = 0, Looping_Unten = 0, Looping_Oben = 0; |
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| 1 | ingob | 107 | |
| 108 | unsigned char Parameter_Luftdruck_D = 48; // Wert : 0-250 |
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| 109 | unsigned char Parameter_MaxHoehe = 251; // Wert : 0-250 |
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| 110 | unsigned char Parameter_Hoehe_P = 16; // Wert : 0-32 |
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| 111 | unsigned char Parameter_Hoehe_ACC_Wirkung = 58; // Wert : 0-250 |
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| 112 | unsigned char Parameter_KompassWirkung = 64; // Wert : 0-250 |
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| 1283 | hbuss | 113 | unsigned char Parameter_Hoehe_GPS_Z = 64; // Wert : 0-250 |
| 1111 | hbuss | 114 | unsigned char Parameter_Gyro_D = 8; // Wert : 0-250 |
| 173 | holgerb | 115 | unsigned char Parameter_Gyro_P = 150; // Wert : 10-250 |
| 1 | ingob | 116 | unsigned char Parameter_Gyro_I = 150; // Wert : 0-250 |
| 1322 | hbuss | 117 | unsigned char Parameter_Gyro_Gier_P = 150; // Wert : 10-250 |
| 118 | unsigned char Parameter_Gyro_Gier_I = 150; // Wert : 10-250 |
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| 1 | ingob | 119 | unsigned char Parameter_Gier_P = 2; // Wert : 1-20 |
| 120 | unsigned char Parameter_I_Faktor = 10; // Wert : 1-20 |
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| 121 | unsigned char Parameter_UserParam1 = 0; |
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| 122 | unsigned char Parameter_UserParam2 = 0; |
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| 123 | unsigned char Parameter_UserParam3 = 0; |
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| 124 | unsigned char Parameter_UserParam4 = 0; |
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| 499 | hbuss | 125 | unsigned char Parameter_UserParam5 = 0; |
| 126 | unsigned char Parameter_UserParam6 = 0; |
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| 127 | unsigned char Parameter_UserParam7 = 0; |
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| 128 | unsigned char Parameter_UserParam8 = 0; |
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| 1 | ingob | 129 | unsigned char Parameter_ServoNickControl = 100; |
| 1232 | hbuss | 130 | unsigned char Parameter_ServoRollControl = 100; |
| 173 | holgerb | 131 | unsigned char Parameter_LoopGasLimit = 70; |
| 1120 | hbuss | 132 | unsigned char Parameter_AchsKopplung1 = 90; |
| 133 | unsigned char Parameter_AchsKopplung2 = 65; |
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| 134 | unsigned char Parameter_CouplingYawCorrection = 64; |
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| 135 | //unsigned char Parameter_AchsGegenKopplung1 = 0; |
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| 499 | hbuss | 136 | unsigned char Parameter_DynamicStability = 100; |
| 921 | hbuss | 137 | unsigned char Parameter_J16Bitmask; // for the J16 Output |
| 138 | unsigned char Parameter_J16Timing; // for the J16 Output |
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| 139 | unsigned char Parameter_J17Bitmask; // for the J17 Output |
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| 140 | unsigned char Parameter_J17Timing; // for the J17 Output |
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| 141 | unsigned char Parameter_NaviGpsModeControl; // Parameters for the Naviboard |
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| 1051 | killagreg | 142 | unsigned char Parameter_NaviGpsGain; |
| 143 | unsigned char Parameter_NaviGpsP; |
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| 144 | unsigned char Parameter_NaviGpsI; |
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| 145 | unsigned char Parameter_NaviGpsD; |
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| 146 | unsigned char Parameter_NaviGpsACC; |
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| 993 | hbuss | 147 | unsigned char Parameter_NaviOperatingRadius; |
| 148 | unsigned char Parameter_NaviWindCorrection; |
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| 149 | unsigned char Parameter_NaviSpeedCompensation; |
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| 921 | hbuss | 150 | unsigned char Parameter_ExternalControl; |
| 1403 | hbuss | 151 | unsigned char Parameter_Servo3,Parameter_Servo4,Parameter_Servo5; |
| 1622 | killagreg | 152 | |
| 492 | hbuss | 153 | signed int ExternStickNick = 0,ExternStickRoll = 0,ExternStickGier = 0, ExternHoehenValue = -20; |
| 614 | hbuss | 154 | int MaxStickNick = 0,MaxStickRoll = 0; |
| 871 | hbuss | 155 | unsigned int modell_fliegt = 0; |
| 1420 | killagreg | 156 | volatile unsigned char FCFlags = 0; |
| 1121 | hbuss | 157 | long GIER_GRAD_FAKTOR = 1291; |
| 1153 | hbuss | 158 | signed int KopplungsteilNickRoll,KopplungsteilRollNick; |
| 1209 | hbuss | 159 | signed int tmp_motorwert[MAX_MOTORS]; |
| 1591 | holgerb | 160 | char VarioCharacter = ' '; |
| 161 | |||
| 1391 | killagreg | 162 | #define LIMIT_MIN(value, min) {if(value <= min) value = min;} |
| 163 | #define LIMIT_MAX(value, max) {if(value >= max) value = max;} |
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| 164 | #define LIMIT_MIN_MAX(value, min, max) {if(value <= min) value = min; else if(value >= max) value = max;} |
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| 1155 | hbuss | 165 | |
| 1622 | killagreg | 166 | |
| 1166 | hbuss | 167 | int MotorSmoothing(int neu, int alt) |
| 168 | { |
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| 169 | int motor; |
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| 170 | if(neu > alt) motor = (1*(int)alt + neu) / 2; |
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| 171 | else motor = neu - (alt - neu)*1; |
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| 172 | //if(Poti2 < 20) return(neu); |
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| 173 | return(motor); |
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| 174 | } |
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| 175 | |||
| 1639 | holgerb | 176 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 177 | // Debugwerte zuordnen |
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| 178 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
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| 179 | void CopyDebugValues(void) |
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| 180 | { |
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| 181 | |||
| 182 | DebugOut.Analog[0] = IntegralNick / (EE_Parameter.GyroAccFaktor * 4); |
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| 183 | DebugOut.Analog[1] = IntegralRoll / (EE_Parameter.GyroAccFaktor * 4); |
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| 184 | DebugOut.Analog[2] = Mittelwert_AccNick / 4; |
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| 185 | DebugOut.Analog[3] = Mittelwert_AccRoll / 4; |
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| 186 | DebugOut.Analog[4] = MesswertGier; |
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| 187 | DebugOut.Analog[5] = HoehenWert/5; |
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| 1643 | holgerb | 188 | DebugOut.Analog[6] = (Mess_Integral_Hoch / 512);//AdWertAccHoch;// Aktuell_az;//(Mess_Integral_Hoch / 512);//Aktuell_az; |
| 1639 | holgerb | 189 | DebugOut.Analog[8] = KompassValue; |
| 190 | DebugOut.Analog[9] = UBat; |
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| 191 | DebugOut.Analog[10] = SenderOkay; |
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| 192 | DebugOut.Analog[11] = ErsatzKompass / GIER_GRAD_FAKTOR; |
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| 193 | DebugOut.Analog[16] = NeutralAccZ; |
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| 194 | //DebugOut.Analog[16] = Motor[0].Temperature; |
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| 195 | //DebugOut.Analog[17] = FromNaviCtrl_Value.Distance; |
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| 196 | // DebugOut.Analog[18] = VarioMeter; |
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| 197 | // DebugOut.Analog[19] = WinkelOut.CalcState; |
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| 198 | DebugOut.Analog[20] = ServoNickValue; |
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| 199 | DebugOut.Analog[22] = Capacity.ActualCurrent; |
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| 200 | DebugOut.Analog[23] = Capacity.UsedCapacity; |
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| 201 | // DebugOut.Analog[22] = FromNaviCtrl_Value.GpsZ; |
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| 202 | // DebugOut.Analog[24] = MesswertNick/2; |
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| 203 | // DebugOut.Analog[25] = MesswertRoll/2; |
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| 204 | // DebugOut.Analog[27] = (int)FromNaviCtrl_Value.Kalman_MaxDrift; |
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| 205 | // DebugOut.Analog[28] = (int)FromNaviCtrl_Value.Kalman_MaxFusion; |
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| 206 | // DebugOut.Analog[29] = (int)FromNaviCtrl_Value.Kalman_K; |
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| 207 | //DebugOut.Analog[28] = I2CError; |
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| 208 | DebugOut.Analog[29] = FromNaviCtrl_Value.SerialDataOkay; |
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| 209 | DebugOut.Analog[30] = GPS_Nick; |
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| 210 | DebugOut.Analog[31] = GPS_Roll; |
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| 211 | } |
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| 212 | |||
| 1232 | hbuss | 213 | void Piep(unsigned char Anzahl, unsigned int dauer) |
| 1 | ingob | 214 | { |
| 1232 | hbuss | 215 | if(MotorenEin) return; //auf keinen Fall im Flug! |
| 1 | ingob | 216 | while(Anzahl--) |
| 217 | { |
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| 1232 | hbuss | 218 | beeptime = dauer; |
| 219 | while(beeptime); |
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| 220 | Delay_ms(dauer * 2); |
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| 1 | ingob | 221 | } |
| 222 | } |
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| 223 | |||
| 224 | //############################################################################ |
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| 1622 | killagreg | 225 | // Messwerte beim Ermitteln der Nullage |
| 226 | void CalibrierMittelwert(void) |
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| 227 | //############################################################################ |
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| 228 | { |
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| 229 | unsigned char i; |
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| 230 | if(PlatinenVersion == 13) SucheGyroOffset(); |
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| 231 | // ADC auschalten, damit die Werte sich nicht während der Berechnung ändern |
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| 232 | ANALOG_OFF; |
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| 233 | MesswertNick = AdWertNick; |
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| 234 | MesswertRoll = AdWertRoll; |
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| 235 | MesswertGier = AdWertGier; |
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| 236 | Mittelwert_AccNick = ACC_AMPLIFY * (long)AdWertAccNick; |
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| 237 | Mittelwert_AccRoll = ACC_AMPLIFY * (long)AdWertAccRoll; |
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| 238 | Mittelwert_AccHoch = (long)AdWertAccHoch; |
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| 239 | // ADC einschalten |
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| 240 | ANALOG_ON; |
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| 241 | for(i=0;i<8;i++) |
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| 242 | { |
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| 243 | int tmp; |
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| 244 | tmp = PPM_in[EE_Parameter.Kanalbelegung[K_POTI1 + i]] + 110; |
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| 245 | LIMIT_MIN_MAX(tmp, 0, 255); |
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| 246 | if(Poti[i] > tmp) Poti[i]--; else if(Poti[i] < tmp) Poti[i]++; |
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| 247 | } |
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| 248 | Umschlag180Nick = (long) EE_Parameter.WinkelUmschlagNick * 2500L; |
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| 249 | Umschlag180Roll = (long) EE_Parameter.WinkelUmschlagRoll * 2500L; |
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| 250 | } |
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| 251 | |||
| 252 | //############################################################################ |
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| 1 | ingob | 253 | // Nullwerte ermitteln |
| 1622 | killagreg | 254 | void SetNeutral(unsigned char AccAdjustment) |
| 1 | ingob | 255 | //############################################################################ |
| 256 | { |
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| 1622 | killagreg | 257 | unsigned char i; |
| 258 | unsigned int gier_neutral=0, nick_neutral=0, roll_neutral=0; |
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| 259 | |||
| 1320 | hbuss | 260 | HEF4017R_ON; |
| 1051 | killagreg | 261 | NeutralAccX = 0; |
| 1 | ingob | 262 | NeutralAccY = 0; |
| 263 | NeutralAccZ = 0; |
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| 1622 | killagreg | 264 | |
| 1051 | killagreg | 265 | AdNeutralNick = 0; |
| 266 | AdNeutralRoll = 0; |
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| 1 | ingob | 267 | AdNeutralGier = 0; |
| 1622 | killagreg | 268 | |
| 395 | hbuss | 269 | Parameter_AchsKopplung1 = 0; |
| 1120 | hbuss | 270 | Parameter_AchsKopplung2 = 0; |
| 1622 | killagreg | 271 | |
| 1036 | hbuss | 272 | ExpandBaro = 0; |
| 1622 | killagreg | 273 | |
| 1648 | killagreg | 274 | I2C_SendBLConfig(); |
| 1639 | holgerb | 275 | |
| 1051 | killagreg | 276 | CalibrierMittelwert(); |
| 395 | hbuss | 277 | Delay_ms_Mess(100); |
| 1622 | killagreg | 278 | |
| 1 | ingob | 279 | CalibrierMittelwert(); |
| 1622 | killagreg | 280 | |
| 1 | ingob | 281 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG)) // Höhenregelung aktiviert? |
| 1051 | killagreg | 282 | { |
| 1 | ingob | 283 | if((MessLuftdruck > 950) || (MessLuftdruck < 750)) SucheLuftruckOffset(); |
| 284 | } |
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| 1166 | hbuss | 285 | #define NEUTRAL_FILTER 32 |
| 286 | for(i=0; i<NEUTRAL_FILTER; i++) |
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| 1111 | hbuss | 287 | { |
| 288 | Delay_ms_Mess(10); |
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| 1216 | killagreg | 289 | gier_neutral += AdWertGier; |
| 1166 | hbuss | 290 | nick_neutral += AdWertNick; |
| 291 | roll_neutral += AdWertRoll; |
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| 1111 | hbuss | 292 | } |
| 1173 | hbuss | 293 | AdNeutralNick= (nick_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER / 8); |
| 294 | AdNeutralRoll= (roll_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER / 8); |
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| 295 | AdNeutralGier= (gier_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER); |
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| 1622 | killagreg | 296 | |
| 401 | hbuss | 297 | StartNeutralRoll = AdNeutralRoll; |
| 298 | StartNeutralNick = AdNeutralNick; |
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| 1622 | killagreg | 299 | |
| 300 | if(AccAdjustment) |
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| 301 | { |
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| 302 | NeutralAccX = abs(Mittelwert_AccNick) / (2*ACC_AMPLIFY); |
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| 303 | NeutralAccY = abs(Mittelwert_AccRoll) / (2*ACC_AMPLIFY); |
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| 304 | NeutralAccZ = Aktuell_az; |
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| 305 | |||
| 306 | // Save ACC neutral settings to eeprom |
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| 1639 | holgerb | 307 | SetParamWord(PID_ACC_NICK, (uint16_t)NeutralAccX); |
| 308 | SetParamWord(PID_ACC_ROLL, (uint16_t)NeutralAccY); |
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| 1622 | killagreg | 309 | SetParamWord(PID_ACC_TOP, (uint16_t)NeutralAccZ); |
| 513 | hbuss | 310 | } |
| 1051 | killagreg | 311 | else |
| 513 | hbuss | 312 | { |
| 1622 | killagreg | 313 | // restore from eeprom |
| 314 | NeutralAccX = (int16_t)GetParamWord(PID_ACC_NICK); |
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| 315 | NeutralAccY = (int16_t)GetParamWord(PID_ACC_ROLL); |
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| 316 | NeutralAccZ = (int16_t)GetParamWord(PID_ACC_TOP); |
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| 317 | // strange settings? |
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| 1638 | holgerb | 318 | if(((unsigned int) NeutralAccX > 2048) || ((unsigned int) NeutralAccY > 2048) || ((unsigned int) NeutralAccZ > 1024)) |
| 1622 | killagreg | 319 | { |
| 320 | printf("\n\rACC not calibrated!\r\n"); |
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| 321 | NeutralAccX = abs(Mittelwert_AccNick) / (2*ACC_AMPLIFY); |
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| 322 | NeutralAccY = abs(Mittelwert_AccRoll) / (2*ACC_AMPLIFY); |
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| 323 | NeutralAccZ = Aktuell_az; |
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| 324 | } |
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| 513 | hbuss | 325 | } |
| 1051 | killagreg | 326 | |
| 1 | ingob | 327 | MesswertNick = 0; |
| 328 | MesswertRoll = 0; |
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| 329 | MesswertGier = 0; |
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| 1111 | hbuss | 330 | Delay_ms_Mess(100); |
| 1174 | hbuss | 331 | Mittelwert_AccNick = ACC_AMPLIFY * (long)AdWertAccNick; |
| 332 | Mittelwert_AccRoll = ACC_AMPLIFY * (long)AdWertAccRoll; |
||
| 1173 | hbuss | 333 | IntegralNick = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccNick; |
| 334 | IntegralRoll = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccRoll; |
||
| 335 | Mess_IntegralNick2 = IntegralNick; |
||
| 336 | Mess_IntegralRoll2 = IntegralRoll; |
||
| 337 | Mess_Integral_Gier = 0; |
||
| 1 | ingob | 338 | StartLuftdruck = Luftdruck; |
| 1253 | killagreg | 339 | VarioMeter = 0; |
| 1 | ingob | 340 | Mess_Integral_Hoch = 0; |
| 341 | KompassStartwert = KompassValue; |
||
| 342 | GPS_Neutral(); |
||
| 1051 | killagreg | 343 | beeptime = 50; |
| 882 | hbuss | 344 | Umschlag180Nick = ((long) EE_Parameter.WinkelUmschlagNick * 2500L) + 15000L; |
| 345 | Umschlag180Roll = ((long) EE_Parameter.WinkelUmschlagRoll * 2500L) + 15000L; |
||
| 492 | hbuss | 346 | ExternHoehenValue = 0; |
| 693 | hbuss | 347 | ErsatzKompass = KompassValue * GIER_GRAD_FAKTOR; |
| 348 | GierGyroFehler = 0; |
||
| 723 | hbuss | 349 | SendVersionToNavi = 1; |
| 921 | hbuss | 350 | LED_Init(); |
| 1420 | killagreg | 351 | FCFlags |= FCFLAG_CALIBRATE; |
| 992 | hbuss | 352 | FromNaviCtrl_Value.Kalman_K = -1; |
| 1173 | hbuss | 353 | FromNaviCtrl_Value.Kalman_MaxDrift = 0; |
| 992 | hbuss | 354 | FromNaviCtrl_Value.Kalman_MaxFusion = 32; |
| 1391 | killagreg | 355 | |
| 356 | for(i=0;i<8;i++) |
||
| 1377 | hbuss | 357 | { |
| 358 | Poti[i] = PPM_in[EE_Parameter.Kanalbelegung[K_POTI1 + i]] + 110; |
||
| 359 | } |
||
| 1171 | hbuss | 360 | SenderOkay = 100; |
| 1320 | hbuss | 361 | if(ServoActive) |
| 362 | { |
||
| 363 | HEF4017R_ON; |
||
| 364 | DDRD |=0x80; // enable J7 -> Servo signal |
||
| 365 | } |
||
| 1 | ingob | 366 | } |
| 367 | |||
| 368 | //############################################################################ |
||
| 395 | hbuss | 369 | // Bearbeitet die Messwerte |
| 1 | ingob | 370 | void Mittelwert(void) |
| 371 | //############################################################################ |
||
| 1051 | killagreg | 372 | { |
| 1111 | hbuss | 373 | static signed long tmpl,tmpl2,tmpl3,tmpl4; |
| 374 | static signed int oldNick, oldRoll, d2Roll, d2Nick; |
||
| 1153 | hbuss | 375 | signed long winkel_nick, winkel_roll; |
| 1377 | hbuss | 376 | unsigned char i; |
| 1111 | hbuss | 377 | MesswertGier = (signed int) AdNeutralGier - AdWertGier; |
| 1171 | hbuss | 378 | MesswertNick = (signed int) AdWertNickFilter / 8; |
| 379 | MesswertRoll = (signed int) AdWertRollFilter / 8; |
||
| 1153 | hbuss | 380 | RohMesswertNick = MesswertNick; |
| 381 | RohMesswertRoll = MesswertRoll; |
||
| 1166 | hbuss | 382 | |
| 395 | hbuss | 383 | // Beschleunigungssensor ++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1166 | hbuss | 384 | Mittelwert_AccNick = ((long)Mittelwert_AccNick * 3 + ((ACC_AMPLIFY * (long)AdWertAccNick))) / 4L; |
| 385 | Mittelwert_AccRoll = ((long)Mittelwert_AccRoll * 3 + ((ACC_AMPLIFY * (long)AdWertAccRoll))) / 4L; |
||
| 386 | Mittelwert_AccHoch = ((long)Mittelwert_AccHoch * 3 + ((long)AdWertAccHoch)) / 4L; |
||
| 395 | hbuss | 387 | IntegralAccNick += ACC_AMPLIFY * AdWertAccNick; |
| 388 | IntegralAccRoll += ACC_AMPLIFY * AdWertAccRoll; |
||
| 805 | hbuss | 389 | NaviAccNick += AdWertAccNick; |
| 390 | NaviAccRoll += AdWertAccRoll; |
||
| 391 | NaviCntAcc++; |
||
| 1153 | hbuss | 392 | IntegralAccZ += Aktuell_az - NeutralAccZ; |
| 393 | |||
| 1155 | hbuss | 394 | //++++++++++++++++++++++++++++++++++++++++++++++++ |
| 395 | // ADC einschalten |
||
| 1171 | hbuss | 396 | ANALOG_ON; |
| 1155 | hbuss | 397 | AdReady = 0; |
| 398 | //++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 399 | |||
| 1216 | killagreg | 400 | if(Mess_IntegralRoll > 93000L) winkel_roll = 93000L; |
| 401 | else if(Mess_IntegralRoll <-93000L) winkel_roll = -93000L; |
||
| 1153 | hbuss | 402 | else winkel_roll = Mess_IntegralRoll; |
| 403 | |||
| 1216 | killagreg | 404 | if(Mess_IntegralNick > 93000L) winkel_nick = 93000L; |
| 405 | else if(Mess_IntegralNick <-93000L) winkel_nick = -93000L; |
||
| 1153 | hbuss | 406 | else winkel_nick = Mess_IntegralNick; |
| 407 | |||
| 1120 | hbuss | 408 | // Gier ++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1153 | hbuss | 409 | Mess_Integral_Gier += MesswertGier; |
| 410 | ErsatzKompass += MesswertGier; |
||
| 395 | hbuss | 411 | // Kopplungsanteil +++++++++++++++++++++++++++++++++++++ |
| 412 | if(!Looping_Nick && !Looping_Roll && (EE_Parameter.GlobalConfig & CFG_ACHSENKOPPLUNG_AKTIV)) |
||
| 413 | { |
||
| 1153 | hbuss | 414 | tmpl3 = (MesswertRoll * winkel_nick) / 2048L; |
| 1120 | hbuss | 415 | tmpl3 *= Parameter_AchsKopplung2; //65 |
| 1111 | hbuss | 416 | tmpl3 /= 4096L; |
| 1153 | hbuss | 417 | tmpl4 = (MesswertNick * winkel_roll) / 2048L; |
| 1216 | killagreg | 418 | tmpl4 *= Parameter_AchsKopplung2; //65 |
| 1111 | hbuss | 419 | tmpl4 /= 4096L; |
| 1153 | hbuss | 420 | KopplungsteilNickRoll = tmpl3; |
| 421 | KopplungsteilRollNick = tmpl4; |
||
| 1111 | hbuss | 422 | tmpl4 -= tmpl3; |
| 423 | ErsatzKompass += tmpl4; |
||
| 1166 | hbuss | 424 | if(!Parameter_CouplingYawCorrection) Mess_Integral_Gier -= tmpl4/2; // Gier nachhelfen |
| 1111 | hbuss | 425 | |
| 1153 | hbuss | 426 | tmpl = ((MesswertGier + tmpl4) * winkel_nick) / 2048L; |
| 1111 | hbuss | 427 | tmpl *= Parameter_AchsKopplung1; // 90 |
| 880 | hbuss | 428 | tmpl /= 4096L; |
| 1153 | hbuss | 429 | tmpl2 = ((MesswertGier + tmpl4) * winkel_roll) / 2048L; |
| 395 | hbuss | 430 | tmpl2 *= Parameter_AchsKopplung1; |
| 880 | hbuss | 431 | tmpl2 /= 4096L; |
| 1225 | hbuss | 432 | if(abs(MesswertGier) > 64) if(labs(tmpl) > 128 || labs(tmpl2) > 128) TrichterFlug = 1; |
| 1153 | hbuss | 433 | //MesswertGier += (Parameter_CouplingYawCorrection * tmpl4) / 256; |
| 395 | hbuss | 434 | } |
| 1166 | hbuss | 435 | else tmpl = tmpl2 = KopplungsteilNickRoll = KopplungsteilRollNick = 0; |
| 1111 | hbuss | 436 | |
| 1166 | hbuss | 437 | TrimRoll = tmpl - tmpl2 / 100L; |
| 438 | TrimNick = -tmpl2 + tmpl / 100L; |
||
| 439 | |||
| 1111 | hbuss | 440 | // Kompasswert begrenzen ++++++++++++++++++++++++++++++++++++++++++++++++ |
| 441 | if(ErsatzKompass >= (360L * GIER_GRAD_FAKTOR)) ErsatzKompass -= 360L * GIER_GRAD_FAKTOR; // 360° Umschlag |
||
| 442 | if(ErsatzKompass < 0) ErsatzKompass += 360L * GIER_GRAD_FAKTOR; |
||
| 395 | hbuss | 443 | // Roll ++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1166 | hbuss | 444 | Mess_IntegralRoll2 += MesswertRoll + TrimRoll; |
| 445 | Mess_IntegralRoll += MesswertRoll + TrimRoll - LageKorrekturRoll; |
||
| 1051 | killagreg | 446 | if(Mess_IntegralRoll > Umschlag180Roll) |
| 395 | hbuss | 447 | { |
| 882 | hbuss | 448 | Mess_IntegralRoll = -(Umschlag180Roll - 25000L); |
| 395 | hbuss | 449 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
| 1051 | killagreg | 450 | } |
| 395 | hbuss | 451 | if(Mess_IntegralRoll <-Umschlag180Roll) |
| 452 | { |
||
| 882 | hbuss | 453 | Mess_IntegralRoll = (Umschlag180Roll - 25000L); |
| 395 | hbuss | 454 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
| 1051 | killagreg | 455 | } |
| 395 | hbuss | 456 | // Nick ++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1166 | hbuss | 457 | Mess_IntegralNick2 += MesswertNick + TrimNick; |
| 458 | Mess_IntegralNick += MesswertNick + TrimNick - LageKorrekturNick; |
||
| 1051 | killagreg | 459 | if(Mess_IntegralNick > Umschlag180Nick) |
| 882 | hbuss | 460 | { |
| 461 | Mess_IntegralNick = -(Umschlag180Nick - 25000L); |
||
| 462 | Mess_IntegralNick2 = Mess_IntegralNick; |
||
| 1051 | killagreg | 463 | } |
| 464 | if(Mess_IntegralNick <-Umschlag180Nick) |
||
| 395 | hbuss | 465 | { |
| 882 | hbuss | 466 | Mess_IntegralNick = (Umschlag180Nick - 25000L); |
| 395 | hbuss | 467 | Mess_IntegralNick2 = Mess_IntegralNick; |
| 1051 | killagreg | 468 | } |
| 1111 | hbuss | 469 | |
| 1 | ingob | 470 | Integral_Gier = Mess_Integral_Gier; |
| 471 | IntegralNick = Mess_IntegralNick; |
||
| 472 | IntegralRoll = Mess_IntegralRoll; |
||
| 1051 | killagreg | 473 | IntegralNick2 = Mess_IntegralNick2; |
| 1 | ingob | 474 | IntegralRoll2 = Mess_IntegralRoll2; |
| 475 | |||
| 1166 | hbuss | 476 | #define D_LIMIT 128 |
| 477 | |||
| 1171 | hbuss | 478 | MesswertNick = HiResNick / 8; |
| 479 | MesswertRoll = HiResRoll / 8; |
||
| 1166 | hbuss | 480 | |
| 1167 | hbuss | 481 | if(AdWertNick < 15) MesswertNick = -1000; if(AdWertNick < 7) MesswertNick = -2000; |
| 482 | if(PlatinenVersion == 10) { if(AdWertNick > 1010) MesswertNick = +1000; if(AdWertNick > 1017) MesswertNick = +2000; } |
||
| 483 | else { if(AdWertNick > 2000) MesswertNick = +1000; if(AdWertNick > 2015) MesswertNick = +2000; } |
||
| 484 | if(AdWertRoll < 15) MesswertRoll = -1000; if(AdWertRoll < 7) MesswertRoll = -2000; |
||
| 485 | if(PlatinenVersion == 10) { if(AdWertRoll > 1010) MesswertRoll = +1000; if(AdWertRoll > 1017) MesswertRoll = +2000; } |
||
| 486 | else { if(AdWertRoll > 2000) MesswertRoll = +1000; if(AdWertRoll > 2015) MesswertRoll = +2000; } |
||
| 487 | |||
| 1216 | killagreg | 488 | if(Parameter_Gyro_D) |
| 1111 | hbuss | 489 | { |
| 1166 | hbuss | 490 | d2Nick = HiResNick - oldNick; |
| 491 | oldNick = (oldNick + HiResNick)/2; |
||
| 1111 | hbuss | 492 | if(d2Nick > D_LIMIT) d2Nick = D_LIMIT; |
| 493 | else if(d2Nick < -D_LIMIT) d2Nick = -D_LIMIT; |
||
| 1166 | hbuss | 494 | MesswertNick += (d2Nick * (signed int) Parameter_Gyro_D) / 16; |
| 495 | d2Roll = HiResRoll - oldRoll; |
||
| 496 | oldRoll = (oldRoll + HiResRoll)/2; |
||
| 1111 | hbuss | 497 | if(d2Roll > D_LIMIT) d2Roll = D_LIMIT; |
| 498 | else if(d2Roll < -D_LIMIT) d2Roll = -D_LIMIT; |
||
| 1166 | hbuss | 499 | MesswertRoll += (d2Roll * (signed int) Parameter_Gyro_D) / 16; |
| 500 | HiResNick += (d2Nick * (signed int) Parameter_Gyro_D); |
||
| 501 | HiResRoll += (d2Roll * (signed int) Parameter_Gyro_D); |
||
| 1216 | killagreg | 502 | } |
| 1111 | hbuss | 503 | |
| 1166 | hbuss | 504 | if(RohMesswertRoll > 0) TrimRoll += ((long) abs(KopplungsteilNickRoll) * Parameter_CouplingYawCorrection) / 64L; |
| 505 | else TrimRoll -= ((long) abs(KopplungsteilNickRoll) * Parameter_CouplingYawCorrection) / 64L; |
||
| 506 | if(RohMesswertNick > 0) TrimNick += ((long) abs(KopplungsteilRollNick) * Parameter_CouplingYawCorrection) / 64L; |
||
| 507 | else TrimNick -= ((long) abs(KopplungsteilRollNick) * Parameter_CouplingYawCorrection) / 64L; |
||
| 1153 | hbuss | 508 | |
| 509 | if(EE_Parameter.GlobalConfig & CFG_DREHRATEN_BEGRENZER && !Looping_Nick && !Looping_Roll) |
||
| 510 | { |
||
| 511 | if(RohMesswertNick > 256) MesswertNick += 1 * (RohMesswertNick - 256); |
||
| 512 | else if(RohMesswertNick < -256) MesswertNick += 1 * (RohMesswertNick + 256); |
||
| 513 | if(RohMesswertRoll > 256) MesswertRoll += 1 * (RohMesswertRoll - 256); |
||
| 514 | else if(RohMesswertRoll < -256) MesswertRoll += 1 * (RohMesswertRoll + 256); |
||
| 515 | } |
||
| 1377 | hbuss | 516 | for(i=0;i<8;i++) |
| 517 | { |
||
| 518 | int tmp; |
||
| 519 | tmp = PPM_in[EE_Parameter.Kanalbelegung[K_POTI1 + i]] + 110; |
||
| 520 | if(tmp > 255) tmp = 255; else if(tmp < 0) tmp = 0; |
||
| 1406 | hbuss | 521 | if(tmp != Poti[i]) |
| 522 | { |
||
| 523 | Poti[i] += (tmp - Poti[i]) / 8; |
||
| 1413 | killagreg | 524 | if(Poti[i] > tmp) Poti[i]--; |
| 1406 | hbuss | 525 | else Poti[i]++; |
| 1413 | killagreg | 526 | } |
| 1377 | hbuss | 527 | } |
| 1 | ingob | 528 | } |
| 529 | |||
| 530 | //############################################################################ |
||
| 531 | // Senden der Motorwerte per I2C-Bus |
||
| 532 | void SendMotorData(void) |
||
| 533 | //############################################################################ |
||
| 1051 | killagreg | 534 | { |
| 1209 | hbuss | 535 | unsigned char i; |
| 921 | hbuss | 536 | if(!MotorenEin) |
| 1 | ingob | 537 | { |
| 1420 | killagreg | 538 | FCFlags &= ~(FCFLAG_MOTOR_RUN | FCFLAG_FLY); |
| 1216 | killagreg | 539 | for(i=0;i<MAX_MOTORS;i++) |
| 540 | { |
||
| 541 | if(!PC_MotortestActive) MotorTest[i] = 0; |
||
| 1638 | holgerb | 542 | Motor[i].SetPoint = MotorTest[i]; |
| 543 | Motor[i].SetPointLowerBits = 0; |
||
| 544 | /* |
||
| 545 | Motor[i].SetPoint = MotorTest[i] / 4; |
||
| 546 | Motor[i].SetPointLowerBits = MotorTest[i] % 4; |
||
| 547 | */ |
||
| 1216 | killagreg | 548 | } |
| 1212 | hbuss | 549 | if(PC_MotortestActive) PC_MotortestActive--; |
| 1216 | killagreg | 550 | } |
| 1420 | killagreg | 551 | else FCFlags |= FCFLAG_MOTOR_RUN; |
| 1111 | hbuss | 552 | |
| 1479 | killagreg | 553 | DebugOut.Analog[12] = Motor[0].SetPoint; |
| 554 | DebugOut.Analog[13] = Motor[1].SetPoint; |
||
| 1521 | killagreg | 555 | DebugOut.Analog[14] = Motor[2].SetPoint; |
| 556 | DebugOut.Analog[15] = Motor[3].SetPoint; |
||
| 1 | ingob | 557 | |
| 558 | //Start I2C Interrupt Mode |
||
| 559 | twi_state = 0; |
||
| 560 | motor = 0; |
||
| 1639 | holgerb | 561 | I2C_Start(); |
| 1 | ingob | 562 | } |
| 563 | |||
| 564 | |||
| 565 | |||
| 566 | //############################################################################ |
||
| 567 | // Trägt ggf. das Poti als Parameter ein |
||
| 1051 | killagreg | 568 | void ParameterZuordnung(void) |
| 1 | ingob | 569 | //############################################################################ |
| 570 | { |
||
| 1391 | killagreg | 571 | #define CHK_POTI(b,a) {if(a < 248) b = a; else b = Poti[255 - a];} |
| 572 | #define CHK_POTI_MM(b,a,min,max) {CHK_POTI(b,a); LIMIT_MIN_MAX(b, min, max);} |
||
| 573 | |||
| 921 | hbuss | 574 | CHK_POTI_MM(Parameter_Luftdruck_D,EE_Parameter.Luftdruck_D,0,100); |
| 575 | CHK_POTI_MM(Parameter_Hoehe_P,EE_Parameter.Hoehe_P,0,100); |
||
| 576 | CHK_POTI_MM(Parameter_Gyro_P,EE_Parameter.Gyro_P,10,255); |
||
| 577 | CHK_POTI_MM(Parameter_J16Timing,EE_Parameter.J16Timing,1,255); |
||
| 578 | CHK_POTI_MM(Parameter_J17Timing,EE_Parameter.J17Timing,1,255); |
||
| 1403 | hbuss | 579 | CHK_POTI(Parameter_Servo3,EE_Parameter.Servo3); |
| 580 | CHK_POTI(Parameter_Servo4,EE_Parameter.Servo4); |
||
| 581 | CHK_POTI(Parameter_Servo5,EE_Parameter.Servo5); |
||
| 1377 | hbuss | 582 | CHK_POTI(Parameter_MaxHoehe,EE_Parameter.MaxHoehe); |
| 1403 | hbuss | 583 | CHK_POTI(Parameter_MaxHoehe,EE_Parameter.MaxHoehe); |
| 1377 | hbuss | 584 | CHK_POTI(Parameter_Hoehe_ACC_Wirkung,EE_Parameter.Hoehe_ACC_Wirkung); |
| 585 | CHK_POTI(Parameter_Hoehe_GPS_Z,EE_Parameter.Hoehe_GPS_Z); |
||
| 586 | CHK_POTI(Parameter_KompassWirkung,EE_Parameter.KompassWirkung); |
||
| 587 | CHK_POTI(Parameter_Gyro_I,EE_Parameter.Gyro_I); |
||
| 588 | CHK_POTI(Parameter_Gyro_D,EE_Parameter.Gyro_D); |
||
| 589 | CHK_POTI(Parameter_Gyro_Gier_P,EE_Parameter.Gyro_Gier_P); |
||
| 590 | CHK_POTI(Parameter_Gyro_Gier_I,EE_Parameter.Gyro_Gier_I); |
||
| 591 | CHK_POTI(Parameter_I_Faktor,EE_Parameter.I_Faktor); |
||
| 592 | CHK_POTI(Parameter_UserParam1,EE_Parameter.UserParam1); |
||
| 593 | CHK_POTI(Parameter_UserParam2,EE_Parameter.UserParam2); |
||
| 594 | CHK_POTI(Parameter_UserParam3,EE_Parameter.UserParam3); |
||
| 595 | CHK_POTI(Parameter_UserParam4,EE_Parameter.UserParam4); |
||
| 596 | CHK_POTI(Parameter_UserParam5,EE_Parameter.UserParam5); |
||
| 597 | CHK_POTI(Parameter_UserParam6,EE_Parameter.UserParam6); |
||
| 598 | CHK_POTI(Parameter_UserParam7,EE_Parameter.UserParam7); |
||
| 599 | CHK_POTI(Parameter_UserParam8,EE_Parameter.UserParam8); |
||
| 600 | CHK_POTI(Parameter_ServoNickControl,EE_Parameter.ServoNickControl); |
||
| 601 | CHK_POTI(Parameter_ServoRollControl,EE_Parameter.ServoRollControl); |
||
| 602 | CHK_POTI(Parameter_LoopGasLimit,EE_Parameter.LoopGasLimit); |
||
| 603 | CHK_POTI(Parameter_AchsKopplung1, EE_Parameter.AchsKopplung1); |
||
| 604 | CHK_POTI(Parameter_AchsKopplung2, EE_Parameter.AchsKopplung2); |
||
| 605 | CHK_POTI(Parameter_CouplingYawCorrection,EE_Parameter.CouplingYawCorrection); |
||
| 606 | // CHK_POTI(Parameter_AchsGegenKopplung1,EE_Parameter.AchsGegenKopplung1,0,255); |
||
| 607 | CHK_POTI(Parameter_DynamicStability,EE_Parameter.DynamicStability); |
||
| 608 | CHK_POTI(Parameter_ExternalControl,EE_Parameter.ExternalControl); |
||
| 1153 | hbuss | 609 | Ki = 10300 / (Parameter_I_Faktor + 1); |
| 1 | ingob | 610 | MAX_GAS = EE_Parameter.Gas_Max; |
| 611 | MIN_GAS = EE_Parameter.Gas_Min; |
||
| 612 | } |
||
| 613 | |||
| 614 | //############################################################################ |
||
| 615 | // |
||
| 616 | void MotorRegler(void) |
||
| 617 | //############################################################################ |
||
| 618 | { |
||
| 1330 | killagreg | 619 | int pd_ergebnis_nick,pd_ergebnis_roll,tmp_int, tmp_int2; |
| 1 | ingob | 620 | int GierMischanteil,GasMischanteil; |
| 621 | static long SummeNick=0,SummeRoll=0; |
||
| 622 | static long sollGier = 0,tmp_long,tmp_long2; |
||
| 395 | hbuss | 623 | static long IntegralFehlerNick = 0; |
| 624 | static long IntegralFehlerRoll = 0; |
||
| 1 | ingob | 625 | static unsigned int RcLostTimer; |
| 626 | static unsigned char delay_neutral = 0; |
||
| 627 | static unsigned char delay_einschalten = 0,delay_ausschalten = 0; |
||
| 1622 | killagreg | 628 | static unsigned char calibration_done = 0; |
| 1 | ingob | 629 | static char NeueKompassRichtungMerken = 0; |
| 395 | hbuss | 630 | static long ausgleichNick, ausgleichRoll; |
| 1153 | hbuss | 631 | int IntegralNickMalFaktor,IntegralRollMalFaktor; |
| 1209 | hbuss | 632 | unsigned char i; |
| 1051 | killagreg | 633 | Mittelwert(); |
| 1 | ingob | 634 | GRN_ON; |
| 1051 | killagreg | 635 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 636 | // Gaswert ermitteln |
| 1051 | killagreg | 637 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 638 | GasMischanteil = StickGas; |
||
| 831 | hbuss | 639 | if(GasMischanteil < MIN_GAS + 10) GasMischanteil = MIN_GAS + 10; |
| 1330 | killagreg | 640 | |
| 1051 | killagreg | 641 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 693 | hbuss | 642 | // Empfang schlecht |
| 1051 | killagreg | 643 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 644 | if(SenderOkay < 100) |
| 645 | { |
||
| 1051 | killagreg | 646 | if(RcLostTimer) RcLostTimer--; |
| 647 | else |
||
| 1 | ingob | 648 | { |
| 649 | MotorenEin = 0; |
||
| 1420 | killagreg | 650 | FCFlags &= ~FCFLAG_NOTLANDUNG; |
| 1051 | killagreg | 651 | } |
| 1 | ingob | 652 | ROT_ON; |
| 693 | hbuss | 653 | if(modell_fliegt > 1000) // wahrscheinlich in der Luft --> langsam absenken |
| 1 | ingob | 654 | { |
| 655 | GasMischanteil = EE_Parameter.NotGas; |
||
| 1420 | killagreg | 656 | FCFlags |= FCFLAG_NOTLANDUNG; |
| 744 | hbuss | 657 | PPM_diff[EE_Parameter.Kanalbelegung[K_NICK]] = 0; |
| 1051 | killagreg | 658 | PPM_diff[EE_Parameter.Kanalbelegung[K_ROLL]] = 0; |
| 1 | ingob | 659 | PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] = 0; |
| 660 | PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] = 0; |
||
| 661 | PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] = 0; |
||
| 173 | holgerb | 662 | } |
| 1 | ingob | 663 | else MotorenEin = 0; |
| 664 | } |
||
| 1051 | killagreg | 665 | else |
| 666 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1 | ingob | 667 | // Emfang gut |
| 1051 | killagreg | 668 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 669 | if(SenderOkay > 140) |
| 670 | { |
||
| 1420 | killagreg | 671 | FCFlags &= ~FCFLAG_NOTLANDUNG; |
| 1 | ingob | 672 | RcLostTimer = EE_Parameter.NotGasZeit * 50; |
| 921 | hbuss | 673 | if(GasMischanteil > 40 && MotorenEin) |
| 1 | ingob | 674 | { |
| 675 | if(modell_fliegt < 0xffff) modell_fliegt++; |
||
| 676 | } |
||
| 871 | hbuss | 677 | if((modell_fliegt < 256)) |
| 1 | ingob | 678 | { |
| 679 | SummeNick = 0; |
||
| 680 | SummeRoll = 0; |
||
| 1051 | killagreg | 681 | if(modell_fliegt == 250) |
| 918 | hbuss | 682 | { |
| 1051 | killagreg | 683 | NeueKompassRichtungMerken = 1; |
| 918 | hbuss | 684 | sollGier = 0; |
| 1051 | killagreg | 685 | Mess_Integral_Gier = 0; |
| 927 | hbuss | 686 | // Mess_Integral_Gier2 = 0; |
| 1051 | killagreg | 687 | } |
| 1420 | killagreg | 688 | } else FCFlags |= FCFLAG_FLY; |
| 1051 | killagreg | 689 | |
| 595 | hbuss | 690 | if((PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] > 80) && MotorenEin == 0) |
| 1 | ingob | 691 | { |
| 1051 | killagreg | 692 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 693 | // auf Nullwerte kalibrieren |
| 1051 | killagreg | 694 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 695 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] > 75) // Neutralwerte |
| 696 | { |
||
| 697 | if(++delay_neutral > 200) // nicht sofort |
||
| 698 | { |
||
| 699 | GRN_OFF; |
||
| 700 | MotorenEin = 0; |
||
| 701 | delay_neutral = 0; |
||
| 702 | modell_fliegt = 0; |
||
| 703 | if(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70 || abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) > 70) |
||
| 704 | { |
||
| 304 | ingob | 705 | unsigned char setting=1; |
| 1 | ingob | 706 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < 70) setting = 1; |
| 707 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 2; |
||
| 708 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 3; |
||
| 709 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] <-70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 4; |
||
| 710 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] <-70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < 70) setting = 5; |
||
| 1622 | killagreg | 711 | SetActiveParamSet(setting); // aktiven Datensatz merken |
| 1 | ingob | 712 | } |
| 820 | hbuss | 713 | // else |
| 1051 | killagreg | 714 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) < 30 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < -70) |
| 715 | { |
||
| 819 | hbuss | 716 | WinkelOut.CalcState = 1; |
| 717 | beeptime = 1000; |
||
| 718 | } |
||
| 719 | else |
||
| 1 | ingob | 720 | { |
| 1622 | killagreg | 721 | ParamSet_ReadFromEEProm(GetActiveParamSet()); |
| 1413 | killagreg | 722 | LipoDetection(0); |
| 1626 | killagreg | 723 | LIBFC_ReceiverInit(EE_Parameter.Receiver); |
| 819 | hbuss | 724 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG)) // Höhenregelung aktiviert? |
| 725 | { |
||
| 1 | ingob | 726 | if((MessLuftdruck > 950) || (MessLuftdruck < 750)) SucheLuftruckOffset(); |
| 1051 | killagreg | 727 | } |
| 1330 | killagreg | 728 | ServoActive = 0; |
| 1622 | killagreg | 729 | SetNeutral(0); |
| 730 | calibration_done = 1; |
||
| 1232 | hbuss | 731 | ServoActive = 1; |
| 732 | DDRD |=0x80; // enable J7 -> Servo signal |
||
| 1622 | killagreg | 733 | Piep(GetActiveParamSet(),120); |
| 819 | hbuss | 734 | } |
| 1051 | killagreg | 735 | } |
| 1 | ingob | 736 | } |
| 1051 | killagreg | 737 | else |
| 513 | hbuss | 738 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] < -75) // ACC Neutralwerte speichern |
| 739 | { |
||
| 740 | if(++delay_neutral > 200) // nicht sofort |
||
| 741 | { |
||
| 742 | GRN_OFF; |
||
| 743 | MotorenEin = 0; |
||
| 744 | delay_neutral = 0; |
||
| 745 | modell_fliegt = 0; |
||
| 1622 | killagreg | 746 | SetNeutral(1); |
| 747 | calibration_done = 1; |
||
| 748 | Piep(GetActiveParamSet(),120); |
||
| 1051 | killagreg | 749 | } |
| 513 | hbuss | 750 | } |
| 1 | ingob | 751 | else delay_neutral = 0; |
| 752 | } |
||
| 1051 | killagreg | 753 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 754 | // Gas ist unten |
| 1051 | killagreg | 755 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 595 | hbuss | 756 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] < 35-120) |
| 1 | ingob | 757 | { |
| 1521 | killagreg | 758 | // Motoren Starten |
| 759 | if(!MotorenEin) |
||
| 760 | { |
||
| 761 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] < -75) |
||
| 762 | { |
||
| 1051 | killagreg | 763 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 764 | // Einschalten |
| 1051 | killagreg | 765 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1521 | killagreg | 766 | if(++delay_einschalten > 200) |
| 767 | { |
||
| 768 | delay_einschalten = 0; |
||
| 1622 | killagreg | 769 | if(calibration_done) |
| 770 | { |
||
| 771 | modell_fliegt = 1; |
||
| 772 | MotorenEin = 1; |
||
| 773 | sollGier = 0; |
||
| 774 | Mess_Integral_Gier = 0; |
||
| 775 | Mess_Integral_Gier2 = 0; |
||
| 776 | Mess_IntegralNick = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccNick; |
||
| 777 | Mess_IntegralRoll = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccRoll; |
||
| 778 | Mess_IntegralNick2 = IntegralNick; |
||
| 779 | Mess_IntegralRoll2 = IntegralRoll; |
||
| 780 | SummeNick = 0; |
||
| 781 | SummeRoll = 0; |
||
| 782 | FCFlags |= FCFLAG_START; |
||
| 783 | } |
||
| 784 | else |
||
| 785 | { |
||
| 786 | beeptime = 1500; // indicate missing calibration |
||
| 787 | } |
||
| 1521 | killagreg | 788 | } |
| 789 | } |
||
| 790 | else delay_einschalten = 0; |
||
| 791 | } |
||
| 1051 | killagreg | 792 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 793 | // Auschalten |
| 1051 | killagreg | 794 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1521 | killagreg | 795 | else // only if motors are running |
| 796 | { |
||
| 797 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] > 75) |
||
| 798 | { |
||
| 799 | if(++delay_ausschalten > 200) // nicht sofort |
||
| 800 | { |
||
| 801 | MotorenEin = 0; |
||
| 802 | delay_ausschalten = 0; |
||
| 803 | modell_fliegt = 0; |
||
| 804 | } |
||
| 805 | } |
||
| 806 | else delay_ausschalten = 0; |
||
| 807 | } |
||
| 1 | ingob | 808 | } |
| 809 | } |
||
| 1051 | killagreg | 810 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 811 | // neue Werte von der Funke |
| 1051 | killagreg | 812 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1216 | killagreg | 813 | |
| 1420 | killagreg | 814 | if(!NewPpmData-- || (FCFlags & FCFLAG_NOTLANDUNG)) |
| 1 | ingob | 815 | { |
| 604 | hbuss | 816 | static int stick_nick,stick_roll; |
| 1 | ingob | 817 | ParameterZuordnung(); |
| 1051 | killagreg | 818 | stick_nick = (stick_nick * 3 + PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] * EE_Parameter.Stick_P) / 4; |
| 723 | hbuss | 819 | stick_nick += PPM_diff[EE_Parameter.Kanalbelegung[K_NICK]] * EE_Parameter.Stick_D; |
| 805 | hbuss | 820 | StickNick = stick_nick - (GPS_Nick + GPS_Nick2); |
| 604 | hbuss | 821 | |
| 723 | hbuss | 822 | stick_roll = (stick_roll * 3 + PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] * EE_Parameter.Stick_P) / 4; |
| 823 | stick_roll += PPM_diff[EE_Parameter.Kanalbelegung[K_ROLL]] * EE_Parameter.Stick_D; |
||
| 805 | hbuss | 824 | StickRoll = stick_roll - (GPS_Roll + GPS_Roll2); |
| 723 | hbuss | 825 | |
| 1 | ingob | 826 | StickGier = -PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]; |
| 1120 | hbuss | 827 | if(StickGier > 2) StickGier -= 2; else |
| 828 | if(StickGier < -2) StickGier += 2; else StickGier = 0; |
||
| 829 | |||
| 1350 | hbuss | 830 | StickGas = PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] + 120; |
| 1330 | killagreg | 831 | |
| 1153 | hbuss | 832 | GyroFaktor = (Parameter_Gyro_P + 10.0); |
| 833 | IntegralFaktor = Parameter_Gyro_I; |
||
| 1322 | hbuss | 834 | GyroFaktorGier = (Parameter_Gyro_Gier_P + 10.0); |
| 835 | IntegralFaktorGier = Parameter_Gyro_Gier_I; |
||
| 1 | ingob | 836 | |
| 595 | hbuss | 837 | //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 838 | //+ Analoge Steuerung per Seriell |
||
| 839 | //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 921 | hbuss | 840 | if(ExternControl.Config & 0x01 && Parameter_ExternalControl > 128) |
| 595 | hbuss | 841 | { |
| 842 | StickNick += (int) ExternControl.Nick * (int) EE_Parameter.Stick_P; |
||
| 843 | StickRoll += (int) ExternControl.Roll * (int) EE_Parameter.Stick_P; |
||
| 844 | StickGier += ExternControl.Gier; |
||
| 845 | ExternHoehenValue = (int) ExternControl.Hight * (int)EE_Parameter.Hoehe_Verstaerkung; |
||
| 846 | if(ExternControl.Gas < StickGas) StickGas = ExternControl.Gas; |
||
| 847 | } |
||
| 855 | hbuss | 848 | if(StickGas < 0) StickGas = 0; |
| 1330 | killagreg | 849 | |
| 1 | ingob | 850 | if(EE_Parameter.GlobalConfig & CFG_HEADING_HOLD) IntegralFaktor = 0; |
| 1330 | killagreg | 851 | //if(GyroFaktor < 0) GyroFaktor = 0; |
| 852 | //if(IntegralFaktor < 0) IntegralFaktor = 0; |
||
| 723 | hbuss | 853 | |
| 1051 | killagreg | 854 | if(abs(StickNick/STICK_GAIN) > MaxStickNick) |
| 928 | hbuss | 855 | { |
| 1051 | killagreg | 856 | MaxStickNick = abs(StickNick)/STICK_GAIN; |
| 928 | hbuss | 857 | if(MaxStickNick > 100) MaxStickNick = 100; |
| 1051 | killagreg | 858 | } |
| 928 | hbuss | 859 | else MaxStickNick--; |
| 1051 | killagreg | 860 | if(abs(StickRoll/STICK_GAIN) > MaxStickRoll) |
| 928 | hbuss | 861 | { |
| 1051 | killagreg | 862 | MaxStickRoll = abs(StickRoll)/STICK_GAIN; |
| 928 | hbuss | 863 | if(MaxStickRoll > 100) MaxStickRoll = 100; |
| 1051 | killagreg | 864 | } |
| 928 | hbuss | 865 | else MaxStickRoll--; |
| 1420 | killagreg | 866 | if(FCFlags & FCFLAG_NOTLANDUNG) {MaxStickNick = 0; MaxStickRoll = 0;} |
| 723 | hbuss | 867 | |
| 1051 | killagreg | 868 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 173 | holgerb | 869 | // Looping? |
| 1051 | killagreg | 870 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 993 | hbuss | 871 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_LINKS) Looping_Links = 1; |
| 1051 | killagreg | 872 | else |
| 873 | { |
||
| 395 | hbuss | 874 | { |
| 1051 | killagreg | 875 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < (EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese))) Looping_Links = 0; |
| 876 | } |
||
| 877 | } |
||
| 993 | hbuss | 878 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < -EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_RECHTS) Looping_Rechts = 1; |
| 1051 | killagreg | 879 | else |
| 395 | hbuss | 880 | { |
| 881 | if(Looping_Rechts) // Hysterese |
||
| 882 | { |
||
| 883 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > -(EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese)) Looping_Rechts = 0; |
||
| 884 | } |
||
| 1051 | killagreg | 885 | } |
| 173 | holgerb | 886 | |
| 993 | hbuss | 887 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_OBEN) Looping_Oben = 1; |
| 1051 | killagreg | 888 | else |
| 889 | { |
||
| 395 | hbuss | 890 | if(Looping_Oben) // Hysterese |
| 891 | { |
||
| 1051 | killagreg | 892 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < (EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese))) Looping_Oben = 0; |
| 893 | } |
||
| 894 | } |
||
| 993 | hbuss | 895 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < -EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_UNTEN) Looping_Unten = 1; |
| 1051 | killagreg | 896 | else |
| 395 | hbuss | 897 | { |
| 898 | if(Looping_Unten) // Hysterese |
||
| 899 | { |
||
| 900 | if(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > -(EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese)) Looping_Unten = 0; |
||
| 901 | } |
||
| 1051 | killagreg | 902 | } |
| 395 | hbuss | 903 | |
| 904 | if(Looping_Links || Looping_Rechts) Looping_Roll = 1; else Looping_Roll = 0; |
||
| 1153 | hbuss | 905 | if(Looping_Oben || Looping_Unten) { Looping_Nick = 1; Looping_Roll = 0; Looping_Links = 0; Looping_Rechts = 0;} else Looping_Nick = 0; |
| 395 | hbuss | 906 | } // Ende neue Funken-Werte |
| 907 | |||
| 908 | if(Looping_Roll || Looping_Nick) |
||
| 909 | { |
||
| 173 | holgerb | 910 | if(GasMischanteil > EE_Parameter.LoopGasLimit) GasMischanteil = EE_Parameter.LoopGasLimit; |
| 1153 | hbuss | 911 | TrichterFlug = 1; |
| 173 | holgerb | 912 | } |
| 913 | |||
| 1051 | killagreg | 914 | |
| 915 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 916 | // Bei Empfangsausfall im Flug |
||
| 917 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1420 | killagreg | 918 | if(FCFlags & FCFLAG_NOTLANDUNG) |
| 1 | ingob | 919 | { |
| 920 | StickGier = 0; |
||
| 921 | StickNick = 0; |
||
| 922 | StickRoll = 0; |
||
| 1211 | hbuss | 923 | GyroFaktor = 90; |
| 924 | IntegralFaktor = 120; |
||
| 925 | GyroFaktorGier = 90; |
||
| 926 | IntegralFaktorGier = 120; |
||
| 173 | holgerb | 927 | Looping_Roll = 0; |
| 928 | Looping_Nick = 0; |
||
| 1051 | killagreg | 929 | } |
| 395 | hbuss | 930 | |
| 931 | |||
| 1051 | killagreg | 932 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 933 | // Integrale auf ACC-Signal abgleichen |
| 1051 | killagreg | 934 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 395 | hbuss | 935 | #define ABGLEICH_ANZAHL 256L |
| 936 | |||
| 937 | MittelIntegralNick += IntegralNick; // Für die Mittelwertbildung aufsummieren |
||
| 938 | MittelIntegralRoll += IntegralRoll; |
||
| 939 | MittelIntegralNick2 += IntegralNick2; |
||
| 940 | MittelIntegralRoll2 += IntegralRoll2; |
||
| 941 | |||
| 942 | if(Looping_Nick || Looping_Roll) |
||
| 943 | { |
||
| 944 | IntegralAccNick = 0; |
||
| 945 | IntegralAccRoll = 0; |
||
| 946 | MittelIntegralNick = 0; |
||
| 947 | MittelIntegralRoll = 0; |
||
| 948 | MittelIntegralNick2 = 0; |
||
| 949 | MittelIntegralRoll2 = 0; |
||
| 950 | Mess_IntegralNick2 = Mess_IntegralNick; |
||
| 951 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
||
| 952 | ZaehlMessungen = 0; |
||
| 498 | hbuss | 953 | LageKorrekturNick = 0; |
| 954 | LageKorrekturRoll = 0; |
||
| 395 | hbuss | 955 | } |
| 956 | |||
| 1051 | killagreg | 957 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1224 | hbuss | 958 | if(!Looping_Nick && !Looping_Roll && (Aktuell_az > 512 || MotorenEin)) |
| 469 | hbuss | 959 | { |
| 960 | long tmp_long, tmp_long2; |
||
| 1171 | hbuss | 961 | if(FromNaviCtrl_Value.Kalman_K != -1 /*&& !TrichterFlug*/) |
| 992 | hbuss | 962 | { |
| 963 | tmp_long = (long)(IntegralNick / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccNick); |
||
| 1051 | killagreg | 964 | tmp_long2 = (long)(IntegralRoll / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccRoll); |
| 965 | tmp_long = (tmp_long * FromNaviCtrl_Value.Kalman_K) / (32 * 16); |
||
| 966 | tmp_long2 = (tmp_long2 * FromNaviCtrl_Value.Kalman_K) / (32 * 16); |
||
| 992 | hbuss | 967 | if((MaxStickNick > 64) || (MaxStickRoll > 64)) |
| 968 | { |
||
| 969 | tmp_long /= 2; |
||
| 970 | tmp_long2 /= 2; |
||
| 971 | } |
||
| 972 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25) |
||
| 973 | { |
||
| 974 | tmp_long /= 3; |
||
| 975 | tmp_long2 /= 3; |
||
| 976 | } |
||
| 977 | if(tmp_long > (long) FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long = (long) FromNaviCtrl_Value.Kalman_MaxFusion; |
||
| 978 | if(tmp_long < (long)-FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long = (long)-FromNaviCtrl_Value.Kalman_MaxFusion; |
||
| 979 | if(tmp_long2 > (long) FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long2 = (long) FromNaviCtrl_Value.Kalman_MaxFusion; |
||
| 980 | if(tmp_long2 < (long)-FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long2 = (long)-FromNaviCtrl_Value.Kalman_MaxFusion; |
||
| 981 | } |
||
| 1051 | killagreg | 982 | else |
| 992 | hbuss | 983 | { |
| 984 | tmp_long = (long)(IntegralNick / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccNick); |
||
| 1051 | killagreg | 985 | tmp_long2 = (long)(IntegralRoll / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccRoll); |
| 992 | hbuss | 986 | tmp_long /= 16; |
| 987 | tmp_long2 /= 16; |
||
| 988 | if((MaxStickNick > 64) || (MaxStickRoll > 64)) |
||
| 989 | { |
||
| 990 | tmp_long /= 3; |
||
| 991 | tmp_long2 /= 3; |
||
| 1216 | killagreg | 992 | } |
| 993 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25) |
||
| 992 | hbuss | 994 | { |
| 995 | tmp_long /= 3; |
||
| 996 | tmp_long2 /= 3; |
||
| 997 | } |
||
| 1155 | hbuss | 998 | |
| 999 | #define AUSGLEICH 32 |
||
| 992 | hbuss | 1000 | if(tmp_long > AUSGLEICH) tmp_long = AUSGLEICH; |
| 1001 | if(tmp_long < -AUSGLEICH) tmp_long =-AUSGLEICH; |
||
| 1002 | if(tmp_long2 > AUSGLEICH) tmp_long2 = AUSGLEICH; |
||
| 1003 | if(tmp_long2 <-AUSGLEICH) tmp_long2 =-AUSGLEICH; |
||
| 1004 | } |
||
| 1166 | hbuss | 1005 | |
| 1006 | //if(Poti2 > 20) { tmp_long = 0; tmp_long2 = 0;} |
||
| 1111 | hbuss | 1007 | Mess_IntegralNick -= tmp_long; |
| 1008 | Mess_IntegralRoll -= tmp_long2; |
||
| 469 | hbuss | 1009 | } |
| 1051 | killagreg | 1010 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 395 | hbuss | 1011 | if(ZaehlMessungen >= ABGLEICH_ANZAHL) |
| 1012 | { |
||
| 1013 | static int cnt = 0; |
||
| 1014 | static char last_n_p,last_n_n,last_r_p,last_r_n; |
||
| 1015 | static long MittelIntegralNick_Alt,MittelIntegralRoll_Alt; |
||
| 1173 | hbuss | 1016 | if(!Looping_Nick && !Looping_Roll && !TrichterFlug && EE_Parameter.Driftkomp) |
| 173 | holgerb | 1017 | { |
| 395 | hbuss | 1018 | MittelIntegralNick /= ABGLEICH_ANZAHL; |
| 1019 | MittelIntegralRoll /= ABGLEICH_ANZAHL; |
||
| 1020 | IntegralAccNick = (EE_Parameter.GyroAccFaktor * IntegralAccNick) / ABGLEICH_ANZAHL; |
||
| 1021 | IntegralAccRoll = (EE_Parameter.GyroAccFaktor * IntegralAccRoll) / ABGLEICH_ANZAHL; |
||
| 1022 | IntegralAccZ = IntegralAccZ / ABGLEICH_ANZAHL; |
||
| 492 | hbuss | 1023 | #define MAX_I 0//(Poti2/10) |
| 395 | hbuss | 1024 | // Nick ++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1025 | IntegralFehlerNick = (long)(MittelIntegralNick - (long)IntegralAccNick); |
||
| 1026 | ausgleichNick = IntegralFehlerNick / EE_Parameter.GyroAccAbgleich; |
||
| 1051 | killagreg | 1027 | // Roll ++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1028 | IntegralFehlerRoll = (long)(MittelIntegralRoll - (long)IntegralAccRoll); |
||
| 395 | hbuss | 1029 | ausgleichRoll = IntegralFehlerRoll / EE_Parameter.GyroAccAbgleich; |
| 614 | hbuss | 1030 | |
| 1031 | LageKorrekturNick = ausgleichNick / ABGLEICH_ANZAHL; |
||
| 498 | hbuss | 1032 | LageKorrekturRoll = ausgleichRoll / ABGLEICH_ANZAHL; |
| 395 | hbuss | 1033 | |
| 992 | hbuss | 1034 | if(((MaxStickNick > 64) || (MaxStickRoll > 64) || (abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25)) && (FromNaviCtrl_Value.Kalman_K == -1)) |
| 614 | hbuss | 1035 | { |
| 1036 | LageKorrekturNick /= 2; |
||
| 720 | ingob | 1037 | LageKorrekturRoll /= 2; |
| 614 | hbuss | 1038 | } |
| 498 | hbuss | 1039 | |
| 1051 | killagreg | 1040 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 395 | hbuss | 1041 | // Gyro-Drift ermitteln |
| 1051 | killagreg | 1042 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 395 | hbuss | 1043 | MittelIntegralNick2 /= ABGLEICH_ANZAHL; |
| 1044 | MittelIntegralRoll2 /= ABGLEICH_ANZAHL; |
||
| 1051 | killagreg | 1045 | tmp_long = IntegralNick2 - IntegralNick; |
| 1046 | tmp_long2 = IntegralRoll2 - IntegralRoll; |
||
| 395 | hbuss | 1047 | //DebugOut.Analog[25] = MittelIntegralRoll2 / 26; |
| 1048 | |||
| 1049 | IntegralFehlerNick = tmp_long; |
||
| 1050 | IntegralFehlerRoll = tmp_long2; |
||
| 1051 | Mess_IntegralNick2 -= IntegralFehlerNick; |
||
| 1052 | Mess_IntegralRoll2 -= IntegralFehlerRoll; |
||
| 1053 | |||
| 1111 | hbuss | 1054 | if(EE_Parameter.Driftkomp) |
| 1055 | { |
||
| 1622 | killagreg | 1056 | if(GierGyroFehler > ABGLEICH_ANZAHL/2) { AdNeutralGier++; } |
| 1057 | if(GierGyroFehler <-ABGLEICH_ANZAHL/2) { AdNeutralGier--; } |
||
| 1111 | hbuss | 1058 | } |
| 693 | hbuss | 1059 | GierGyroFehler = 0; |
| 720 | ingob | 1060 | |
| 1061 | |||
| 1243 | killagreg | 1062 | #define FEHLER_LIMIT (ABGLEICH_ANZAHL / 2) |
| 1063 | #define FEHLER_LIMIT1 (ABGLEICH_ANZAHL * 2) //4 |
||
| 1225 | hbuss | 1064 | #define FEHLER_LIMIT2 (ABGLEICH_ANZAHL * 16) //16 |
| 492 | hbuss | 1065 | #define BEWEGUNGS_LIMIT 20000 |
| 395 | hbuss | 1066 | // Nick +++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1067 | cnt = 1;// + labs(IntegralFehlerNick) / 4096; |
||
| 1225 | hbuss | 1068 | if(labs(IntegralFehlerNick) > FEHLER_LIMIT1) cnt = 4; |
| 1173 | hbuss | 1069 | if(labs(MittelIntegralNick_Alt - MittelIntegralNick) < BEWEGUNGS_LIMIT || (FromNaviCtrl_Value.Kalman_MaxDrift > 3*8)) |
| 492 | hbuss | 1070 | { |
| 1051 | killagreg | 1071 | if(IntegralFehlerNick > FEHLER_LIMIT2) |
| 395 | hbuss | 1072 | { |
| 1051 | killagreg | 1073 | if(last_n_p) |
| 395 | hbuss | 1074 | { |
| 1173 | hbuss | 1075 | cnt += labs(IntegralFehlerNick) / (FEHLER_LIMIT2 / 8); |
| 492 | hbuss | 1076 | ausgleichNick = IntegralFehlerNick / 8; |
| 401 | hbuss | 1077 | if(ausgleichNick > 5000) ausgleichNick = 5000; |
| 498 | hbuss | 1078 | LageKorrekturNick += ausgleichNick / ABGLEICH_ANZAHL; |
| 1051 | killagreg | 1079 | } |
| 395 | hbuss | 1080 | else last_n_p = 1; |
| 1081 | } else last_n_p = 0; |
||
| 1051 | killagreg | 1082 | if(IntegralFehlerNick < -FEHLER_LIMIT2) |
| 395 | hbuss | 1083 | { |
| 1084 | if(last_n_n) |
||
| 1051 | killagreg | 1085 | { |
| 1173 | hbuss | 1086 | cnt += labs(IntegralFehlerNick) / (FEHLER_LIMIT2 / 8); |
| 492 | hbuss | 1087 | ausgleichNick = IntegralFehlerNick / 8; |
| 401 | hbuss | 1088 | if(ausgleichNick < -5000) ausgleichNick = -5000; |
| 498 | hbuss | 1089 | LageKorrekturNick += ausgleichNick / ABGLEICH_ANZAHL; |
| 1051 | killagreg | 1090 | } |
| 395 | hbuss | 1091 | else last_n_n = 1; |
| 1092 | } else last_n_n = 0; |
||
| 1051 | killagreg | 1093 | } |
| 1094 | else |
||
| 847 | hbuss | 1095 | { |
| 1096 | cnt = 0; |
||
| 921 | hbuss | 1097 | KompassSignalSchlecht = 1000; |
| 1051 | killagreg | 1098 | } |
| 499 | hbuss | 1099 | if(cnt > EE_Parameter.Driftkomp) cnt = EE_Parameter.Driftkomp; |
| 1173 | hbuss | 1100 | if(FromNaviCtrl_Value.Kalman_MaxDrift) if(cnt > FromNaviCtrl_Value.Kalman_MaxDrift) cnt = FromNaviCtrl_Value.Kalman_MaxDrift; |
| 395 | hbuss | 1101 | if(IntegralFehlerNick > FEHLER_LIMIT) AdNeutralNick += cnt; |
| 1102 | if(IntegralFehlerNick < -FEHLER_LIMIT) AdNeutralNick -= cnt; |
||
| 401 | hbuss | 1103 | |
| 395 | hbuss | 1104 | // Roll +++++++++++++++++++++++++++++++++++++++++++++++++ |
| 492 | hbuss | 1105 | cnt = 1;// + labs(IntegralFehlerNick) / 4096; |
| 1225 | hbuss | 1106 | if(labs(IntegralFehlerRoll) > FEHLER_LIMIT1) cnt = 4; |
| 498 | hbuss | 1107 | ausgleichRoll = 0; |
| 1173 | hbuss | 1108 | if(labs(MittelIntegralRoll_Alt - MittelIntegralRoll) < BEWEGUNGS_LIMIT || (FromNaviCtrl_Value.Kalman_MaxDrift > 3*8)) |
| 492 | hbuss | 1109 | { |
| 1051 | killagreg | 1110 | if(IntegralFehlerRoll > FEHLER_LIMIT2) |
| 395 | hbuss | 1111 | { |
| 1051 | killagreg | 1112 | if(last_r_p) |
| 395 | hbuss | 1113 | { |
| 1173 | hbuss | 1114 | cnt += labs(IntegralFehlerRoll) / (FEHLER_LIMIT2 / 8); |
| 492 | hbuss | 1115 | ausgleichRoll = IntegralFehlerRoll / 8; |
| 401 | hbuss | 1116 | if(ausgleichRoll > 5000) ausgleichRoll = 5000; |
| 498 | hbuss | 1117 | LageKorrekturRoll += ausgleichRoll / ABGLEICH_ANZAHL; |
| 1051 | killagreg | 1118 | } |
| 395 | hbuss | 1119 | else last_r_p = 1; |
| 1120 | } else last_r_p = 0; |
||
| 1051 | killagreg | 1121 | if(IntegralFehlerRoll < -FEHLER_LIMIT2) |
| 395 | hbuss | 1122 | { |
| 1051 | killagreg | 1123 | if(last_r_n) |
| 395 | hbuss | 1124 | { |
| 1173 | hbuss | 1125 | cnt += labs(IntegralFehlerRoll) / (FEHLER_LIMIT2 / 8); |
| 492 | hbuss | 1126 | ausgleichRoll = IntegralFehlerRoll / 8; |
| 401 | hbuss | 1127 | if(ausgleichRoll < -5000) ausgleichRoll = -5000; |
| 498 | hbuss | 1128 | LageKorrekturRoll += ausgleichRoll / ABGLEICH_ANZAHL; |
| 395 | hbuss | 1129 | } |
| 1130 | else last_r_n = 1; |
||
| 1131 | } else last_r_n = 0; |
||
| 1051 | killagreg | 1132 | } else |
| 492 | hbuss | 1133 | { |
| 1134 | cnt = 0; |
||
| 921 | hbuss | 1135 | KompassSignalSchlecht = 1000; |
| 1051 | killagreg | 1136 | } |
| 499 | hbuss | 1137 | if(cnt > EE_Parameter.Driftkomp) cnt = EE_Parameter.Driftkomp; |
| 1173 | hbuss | 1138 | if(FromNaviCtrl_Value.Kalman_MaxDrift) if(cnt > FromNaviCtrl_Value.Kalman_MaxDrift) cnt = FromNaviCtrl_Value.Kalman_MaxDrift; |
| 395 | hbuss | 1139 | if(IntegralFehlerRoll > FEHLER_LIMIT) AdNeutralRoll += cnt; |
| 1140 | if(IntegralFehlerRoll < -FEHLER_LIMIT) AdNeutralRoll -= cnt; |
||
| 173 | holgerb | 1141 | } |
| 1051 | killagreg | 1142 | else |
| 498 | hbuss | 1143 | { |
| 1144 | LageKorrekturRoll = 0; |
||
| 1145 | LageKorrekturNick = 0; |
||
| 880 | hbuss | 1146 | TrichterFlug = 0; |
| 498 | hbuss | 1147 | } |
| 1051 | killagreg | 1148 | |
| 498 | hbuss | 1149 | if(!IntegralFaktor) { LageKorrekturRoll = 0; LageKorrekturNick = 0;} // z.B. bei HH |
| 1051 | killagreg | 1150 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1151 | MittelIntegralNick_Alt = MittelIntegralNick; |
||
| 1152 | MittelIntegralRoll_Alt = MittelIntegralRoll; |
||
| 1153 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 395 | hbuss | 1154 | IntegralAccNick = 0; |
| 1155 | IntegralAccRoll = 0; |
||
| 1156 | IntegralAccZ = 0; |
||
| 1157 | MittelIntegralNick = 0; |
||
| 1158 | MittelIntegralRoll = 0; |
||
| 1159 | MittelIntegralNick2 = 0; |
||
| 1160 | MittelIntegralRoll2 = 0; |
||
| 1161 | ZaehlMessungen = 0; |
||
| 1173 | hbuss | 1162 | } // ZaehlMessungen >= ABGLEICH_ANZAHL |
| 395 | hbuss | 1163 | |
| 1051 | killagreg | 1164 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 1165 | // Gieren |
| 1051 | killagreg | 1166 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 693 | hbuss | 1167 | // if(GasMischanteil < 35) { if(StickGier > 10) StickGier = 10; else if(StickGier < -10) StickGier = -10;}; |
| 1051 | killagreg | 1168 | if(abs(StickGier) > 15) // war 35 |
| 1 | ingob | 1169 | { |
| 921 | hbuss | 1170 | KompassSignalSchlecht = 1000; |
| 1051 | killagreg | 1171 | if(!(EE_Parameter.GlobalConfig & CFG_KOMPASS_FIX)) |
| 1172 | { |
||
| 1173 | NeueKompassRichtungMerken = 1; |
||
| 824 | hbuss | 1174 | }; |
| 1 | ingob | 1175 | } |
| 395 | hbuss | 1176 | tmp_int = (long) EE_Parameter.Gier_P * ((long)StickGier * abs(StickGier)) / 512L; // expo y = ax + bx² |
| 1051 | killagreg | 1177 | tmp_int += (EE_Parameter.Gier_P * StickGier) / 4; |
| 173 | holgerb | 1178 | sollGier = tmp_int; |
| 1051 | killagreg | 1179 | Mess_Integral_Gier -= tmp_int; |
| 395 | hbuss | 1180 | if(Mess_Integral_Gier > 50000) Mess_Integral_Gier = 50000; // begrenzen |
| 1181 | if(Mess_Integral_Gier <-50000) Mess_Integral_Gier =-50000; |
||
| 1051 | killagreg | 1182 | |
| 1183 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1 | ingob | 1184 | // Kompass |
| 1051 | killagreg | 1185 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1175 | hbuss | 1186 | //DebugOut.Analog[16] = KompassSignalSchlecht; |
| 819 | hbuss | 1187 | |
| 1051 | killagreg | 1188 | if(KompassValue && (EE_Parameter.GlobalConfig & CFG_KOMPASS_AKTIV)) |
| 1 | ingob | 1189 | { |
| 819 | hbuss | 1190 | int w,v,r,fehler,korrektur; |
| 1 | ingob | 1191 | w = abs(IntegralNick /512); // mit zunehmender Neigung den Einfluss drosseln |
| 1192 | v = abs(IntegralRoll /512); |
||
| 1193 | if(v > w) w = v; // grösste Neigung ermitteln |
||
| 824 | hbuss | 1194 | korrektur = w / 8 + 1; |
| 921 | hbuss | 1195 | fehler = ((540 + KompassValue - (ErsatzKompass/GIER_GRAD_FAKTOR)) % 360) - 180; |
| 1171 | hbuss | 1196 | if(abs(MesswertGier) > 128) |
| 1036 | hbuss | 1197 | { |
| 1198 | fehler = 0; |
||
| 1051 | killagreg | 1199 | } |
| 921 | hbuss | 1200 | if(!KompassSignalSchlecht && w < 25) |
| 1201 | { |
||
| 1202 | GierGyroFehler += fehler; |
||
| 1051 | killagreg | 1203 | if(NeueKompassRichtungMerken) |
| 1204 | { |
||
| 1352 | hbuss | 1205 | // beeptime = 200; |
| 847 | hbuss | 1206 | // KompassStartwert = KompassValue; |
| 1171 | hbuss | 1207 | ErsatzKompass = KompassValue * GIER_GRAD_FAKTOR; |
| 921 | hbuss | 1208 | KompassStartwert = (ErsatzKompass/GIER_GRAD_FAKTOR); |
| 1209 | NeueKompassRichtungMerken = 0; |
||
| 1210 | } |
||
| 1 | ingob | 1211 | } |
| 824 | hbuss | 1212 | ErsatzKompass += (fehler * 8) / korrektur; |
| 921 | hbuss | 1213 | w = (w * Parameter_KompassWirkung) / 32; // auf die Wirkung normieren |
| 1 | ingob | 1214 | w = Parameter_KompassWirkung - w; // Wirkung ggf drosseln |
| 921 | hbuss | 1215 | if(w >= 0) |
| 1 | ingob | 1216 | { |
| 1051 | killagreg | 1217 | if(!KompassSignalSchlecht) |
| 693 | hbuss | 1218 | { |
| 1051 | killagreg | 1219 | v = 64 + ((MaxStickNick + MaxStickRoll)) / 8; |
| 847 | hbuss | 1220 | r = ((540 + (ErsatzKompass/GIER_GRAD_FAKTOR) - KompassStartwert) % 360) - 180; |
| 1221 | // r = KompassRichtung; |
||
| 819 | hbuss | 1222 | v = (r * w) / v; // nach Kompass ausrichten |
| 1223 | w = 3 * Parameter_KompassWirkung; |
||
| 693 | hbuss | 1224 | if(v > w) v = w; // Begrenzen |
| 1051 | killagreg | 1225 | else |
| 693 | hbuss | 1226 | if(v < -w) v = -w; |
| 1227 | Mess_Integral_Gier += v; |
||
| 1051 | killagreg | 1228 | } |
| 693 | hbuss | 1229 | if(KompassSignalSchlecht) KompassSignalSchlecht--; |
| 1051 | killagreg | 1230 | } |
| 921 | hbuss | 1231 | else KompassSignalSchlecht = 500; // so lange das Signal taub stellen --> ca. 1 sek |
| 1051 | killagreg | 1232 | } |
| 1 | ingob | 1233 | |
| 1051 | killagreg | 1234 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 1235 | // Drehgeschwindigkeit und -winkel zu einem Istwert zusammenfassen |
| 1051 | killagreg | 1236 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1216 | killagreg | 1237 | if(TrichterFlug) { SummeRoll = 0; SummeNick = 0;}; |
| 604 | hbuss | 1238 | |
| 1171 | hbuss | 1239 | if(!Looping_Nick) IntegralNickMalFaktor = (IntegralNick * IntegralFaktor) / (44000 / STICK_GAIN); else IntegralNickMalFaktor = 0; |
| 1240 | if(!Looping_Roll) IntegralRollMalFaktor = (IntegralRoll * IntegralFaktor) / (44000 / STICK_GAIN); else IntegralRollMalFaktor = 0; |
||
| 1153 | hbuss | 1241 | |
| 1167 | hbuss | 1242 | #define TRIM_MAX 200 |
| 1166 | hbuss | 1243 | if(TrimNick > TRIM_MAX) TrimNick = TRIM_MAX; else if(TrimNick <-TRIM_MAX) TrimNick =-TRIM_MAX; |
| 1244 | if(TrimRoll > TRIM_MAX) TrimRoll = TRIM_MAX; else if(TrimRoll <-TRIM_MAX) TrimRoll =-TRIM_MAX; |
||
| 1153 | hbuss | 1245 | |
| 1166 | hbuss | 1246 | MesswertNick = IntegralNickMalFaktor + (long)((long)MesswertNick * GyroFaktor + (long)TrimNick * 128L) / (256L / STICK_GAIN); |
| 1247 | MesswertRoll = IntegralRollMalFaktor + (long)((long)MesswertRoll * GyroFaktor + (long)TrimRoll * 128L) / (256L / STICK_GAIN); |
||
| 1211 | hbuss | 1248 | MesswertGier = (long)(MesswertGier * 2 * (long)GyroFaktorGier) / (256L / STICK_GAIN) + (long)(Integral_Gier * IntegralFaktorGier) / (2 * (44000 / STICK_GAIN)); |
| 1166 | hbuss | 1249 | |
| 1 | ingob | 1250 | // Maximalwerte abfangen |
| 1153 | hbuss | 1251 | // #define MAX_SENSOR (4096*STICK_GAIN) |
| 1252 | #define MAX_SENSOR (4096*4) |
||
| 1216 | killagreg | 1253 | if(MesswertNick > MAX_SENSOR) MesswertNick = MAX_SENSOR; |
| 1 | ingob | 1254 | if(MesswertNick < -MAX_SENSOR) MesswertNick = -MAX_SENSOR; |
| 1255 | if(MesswertRoll > MAX_SENSOR) MesswertRoll = MAX_SENSOR; |
||
| 1256 | if(MesswertRoll < -MAX_SENSOR) MesswertRoll = -MAX_SENSOR; |
||
| 1257 | if(MesswertGier > MAX_SENSOR) MesswertGier = MAX_SENSOR; |
||
| 1258 | if(MesswertGier < -MAX_SENSOR) MesswertGier = -MAX_SENSOR; |
||
| 1259 | |||
| 1051 | killagreg | 1260 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 1261 | // Höhenregelung |
| 1262 | // Die Höhenregelung schwächt lediglich das Gas ab, erhöht es allerdings nicht |
||
| 1051 | killagreg | 1263 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1374 | hbuss | 1264 | if(UBat > BattLowVoltageWarning) GasMischanteil = ((unsigned int)GasMischanteil * BattLowVoltageWarning) / UBat; // Gas auf das aktuelle Spannungvieveau beziehen |
| 855 | hbuss | 1265 | GasMischanteil *= STICK_GAIN; |
| 1309 | hbuss | 1266 | // if height control is activated |
| 1322 | hbuss | 1267 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG) && !(Looping_Roll || Looping_Nick)) // Höhenregelung |
| 1309 | hbuss | 1268 | { |
| 1590 | killagreg | 1269 | #define HOVER_GAS_AVERAGE 4096L // 4096 * 2ms = 8.2s averaging |
| 1332 | hbuss | 1270 | #define HC_GAS_AVERAGE 4 // 4 * 2ms= 8ms averaging |
| 1638 | holgerb | 1271 | |
| 1272 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
||
| 1273 | #define OPA_OFFSET_STEP 15 |
||
| 1642 | killagreg | 1274 | #else |
| 1638 | holgerb | 1275 | #define OPA_OFFSET_STEP 10 |
| 1276 | #endif |
||
| 1587 | killagreg | 1277 | int HCGas, HeightDeviation = 0; |
| 1309 | hbuss | 1278 | static int HeightTrimming = 0; // rate for change of height setpoint |
| 1279 | static int FilterHCGas = 0; |
||
| 1587 | killagreg | 1280 | static int StickGasHover = 120, HoverGas = 0, HoverGasMin = 0, HoverGasMax = 1023; |
| 1281 | static unsigned long HoverGasFilter = 0; |
||
| 1322 | hbuss | 1282 | static unsigned char delay = 100, BaroAtUpperLimit = 0, BaroAtLowerLimit = 0; |
| 1320 | hbuss | 1283 | int CosAttitude; // for projection of hoover gas |
| 1330 | killagreg | 1284 | |
| 1309 | hbuss | 1285 | // get the current hooverpoint |
| 1587 | killagreg | 1286 | DebugOut.Analog[21] = HoverGas; |
| 1642 | killagreg | 1287 | |
| 1322 | hbuss | 1288 | // Expand the measurement |
| 1289 | // measurement of air pressure close to upper limit and no overflow in correction of the new OCR0A value occurs |
||
| 1290 | if(!BaroExpandActive) |
||
| 1291 | { |
||
| 1292 | if(MessLuftdruck > 920) |
||
| 1293 | { // increase offset |
||
| 1330 | killagreg | 1294 | if(OCR0A < (255 - OPA_OFFSET_STEP)) |
| 1322 | hbuss | 1295 | { |
| 1296 | ExpandBaro -= 1; |
||
| 1297 | OCR0A = DruckOffsetSetting - OPA_OFFSET_STEP * ExpandBaro; // increase offset to shift ADC down |
||
| 1298 | beeptime = 300; |
||
| 1352 | hbuss | 1299 | BaroExpandActive = 350; |
| 1330 | killagreg | 1300 | } |
| 1301 | else |
||
| 1322 | hbuss | 1302 | { |
| 1303 | BaroAtLowerLimit = 1; |
||
| 1304 | } |
||
| 1305 | } |
||
| 1306 | // measurement of air pressure close to lower limit and |
||
| 1330 | killagreg | 1307 | else |
| 1322 | hbuss | 1308 | if(MessLuftdruck < 100) |
| 1309 | { // decrease offset |
||
| 1330 | killagreg | 1310 | if(OCR0A > OPA_OFFSET_STEP) |
| 1322 | hbuss | 1311 | { |
| 1312 | ExpandBaro += 1; |
||
| 1313 | OCR0A = DruckOffsetSetting - OPA_OFFSET_STEP * ExpandBaro; // decrease offset to shift ADC up |
||
| 1314 | beeptime = 300; |
||
| 1352 | hbuss | 1315 | BaroExpandActive = 350; |
| 1330 | killagreg | 1316 | } |
| 1317 | else |
||
| 1322 | hbuss | 1318 | { |
| 1319 | BaroAtUpperLimit = 1; |
||
| 1320 | } |
||
| 1321 | } |
||
| 1330 | killagreg | 1322 | else |
| 1322 | hbuss | 1323 | { |
| 1324 | BaroAtUpperLimit = 0; |
||
| 1325 | BaroAtLowerLimit = 0; |
||
| 1326 | } |
||
| 1327 | } |
||
| 1328 | else // delay, because of expanding the Baro-Range |
||
| 1329 | { |
||
| 1330 | // now clear the D-values |
||
| 1331 | SummenHoehe = HoehenWert * SM_FILTER; |
||
| 1332 | VarioMeter = 0; |
||
| 1333 | BaroExpandActive--; |
||
| 1334 | } |
||
| 1328 | hbuss | 1335 | |
| 1336 | // if height control is activated by an rc channel |
||
| 1337 | if(EE_Parameter.GlobalConfig & CFG_HOEHEN_SCHALTER) // Regler wird über Schalter gesteuert |
||
| 1338 | { // check if parameter is less than activation threshold |
||
| 1339 | if(Parameter_MaxHoehe < 50) // for 3 or 2-state switch height control is disabled in lowest position |
||
| 1340 | { //height control not active |
||
| 1341 | if(!delay--) |
||
| 1342 | { |
||
| 1343 | HoehenReglerAktiv = 0; // disable height control |
||
| 1344 | SollHoehe = HoehenWert; // update SetPoint with current reading |
||
| 1345 | delay = 1; |
||
| 1346 | } |
||
| 1347 | } |
||
| 1348 | else |
||
| 1349 | { //height control is activated |
||
| 1350 | HoehenReglerAktiv = 1; // enable height control |
||
| 1334 | killagreg | 1351 | delay = 200; |
| 1328 | hbuss | 1352 | } |
| 1051 | killagreg | 1353 | } |
| 1309 | hbuss | 1354 | else // no switchable height control |
| 1355 | { |
||
| 1356 | SollHoehe = ((int16_t) ExternHoehenValue + (int16_t) Parameter_MaxHoehe) * (int)EE_Parameter.Hoehe_Verstaerkung; |
||
| 1357 | HoehenReglerAktiv = 1; |
||
| 1051 | killagreg | 1358 | } |
| 1322 | hbuss | 1359 | |
| 1320 | hbuss | 1360 | // calculate cos of nick and roll angle used for projection of the vertical hoover gas |
| 1330 | killagreg | 1361 | tmp_int = (int)(IntegralNick/GIER_GRAD_FAKTOR); // nick angle in deg |
| 1362 | tmp_int2 = (int)(IntegralRoll/GIER_GRAD_FAKTOR); // roll angle in deg |
||
| 1363 | CosAttitude = (int16_t)ihypot(tmp_int, tmp_int2); // phytagoras gives effective attitude angle in deg |
||
| 1320 | hbuss | 1364 | LIMIT_MAX(CosAttitude, 60); // limit effective attitude angle |
| 1365 | CosAttitude = c_cos_8192(CosAttitude); // cos of actual attitude |
||
| 1591 | holgerb | 1366 | VarioCharacter = ' '; |
| 1420 | killagreg | 1367 | if(HoehenReglerAktiv && !(FCFlags & FCFLAG_NOTLANDUNG)) |
| 1309 | hbuss | 1368 | { |
| 1369 | #define HEIGHT_TRIM_UP 0x01 |
||
| 1370 | #define HEIGHT_TRIM_DOWN 0x02 |
||
| 1371 | static unsigned char HeightTrimmingFlag = 0x00; |
||
| 1372 | |||
| 1330 | killagreg | 1373 | #define HEIGHT_CONTROL_STICKTHRESHOLD 15 |
| 1309 | hbuss | 1374 | // Holger original version |
| 1375 | // start of height control algorithm |
||
| 1376 | // the height control is only an attenuation of the actual gas stick. |
||
| 1377 | // I.e. it will work only if the gas stick is higher than the hover gas |
||
| 1378 | // and the hover height will be allways larger than height setpoint. |
||
| 1314 | killagreg | 1379 | if((EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT) || !(EE_Parameter.GlobalConfig & CFG_HOEHEN_SCHALTER)) // Regler wird über Schalter gesteuert) |
| 1380 | { // old version |
||
| 1309 | hbuss | 1381 | HCGas = GasMischanteil; // take current stick gas as neutral point for the height control |
| 1382 | HeightTrimming = 0; |
||
| 1383 | } |
||
| 1314 | killagreg | 1384 | else |
| 1309 | hbuss | 1385 | { |
| 1386 | // alternative height control |
||
| 1387 | // PD-Control with respect to hoover point |
||
| 1388 | // the thrust loss out of horizontal attitude is compensated |
||
| 1389 | // the setpoint will be fine adjusted with the gas stick position |
||
| 1420 | killagreg | 1390 | if(FCFlags & FCFLAG_FLY) // trim setpoint only when flying |
| 1309 | hbuss | 1391 | { // gas stick is above hoover point |
| 1587 | killagreg | 1392 | if(StickGas > (StickGasHover + HEIGHT_CONTROL_STICKTHRESHOLD) && !BaroAtUpperLimit) |
| 1309 | hbuss | 1393 | { |
| 1394 | if(HeightTrimmingFlag & HEIGHT_TRIM_DOWN) |
||
| 1395 | { |
||
| 1396 | HeightTrimmingFlag &= ~HEIGHT_TRIM_DOWN; |
||
| 1397 | SollHoehe = HoehenWert; // update setpoint to current heigth |
||
| 1398 | } |
||
| 1399 | HeightTrimmingFlag |= HEIGHT_TRIM_UP; |
||
| 1587 | killagreg | 1400 | HeightTrimming += abs(StickGas - (StickGasHover + HEIGHT_CONTROL_STICKTHRESHOLD)); |
| 1591 | holgerb | 1401 | VarioCharacter = '+'; |
| 1309 | hbuss | 1402 | } // gas stick is below hoover point |
| 1587 | killagreg | 1403 | else if(StickGas < (StickGasHover - HEIGHT_CONTROL_STICKTHRESHOLD) && !BaroAtLowerLimit ) |
| 1309 | hbuss | 1404 | { |
| 1405 | if(HeightTrimmingFlag & HEIGHT_TRIM_UP) |
||
| 1406 | { |
||
| 1407 | HeightTrimmingFlag &= ~HEIGHT_TRIM_UP; |
||
| 1408 | SollHoehe = HoehenWert; // update setpoint to current heigth |
||
| 1409 | } |
||
| 1410 | HeightTrimmingFlag |= HEIGHT_TRIM_DOWN; |
||
| 1587 | killagreg | 1411 | HeightTrimming -= abs(StickGas - (StickGasHover - HEIGHT_CONTROL_STICKTHRESHOLD)); |
| 1591 | holgerb | 1412 | VarioCharacter = '-'; |
| 1309 | hbuss | 1413 | } |
| 1587 | killagreg | 1414 | else // Gas Stick in Hover Range |
| 1309 | hbuss | 1415 | { |
| 1352 | hbuss | 1416 | if(HeightTrimmingFlag & (HEIGHT_TRIM_UP | HEIGHT_TRIM_DOWN)) |
| 1309 | hbuss | 1417 | { |
| 1352 | hbuss | 1418 | HeightTrimmingFlag &= ~(HEIGHT_TRIM_UP | HEIGHT_TRIM_DOWN); |
| 1309 | hbuss | 1419 | HeightTrimming = 0; |
| 1420 | SollHoehe = HoehenWert; // update setpoint to current height |
||
| 1421 | if(EE_Parameter.ExtraConfig & CFG2_VARIO_BEEP) beeptime = 500; |
||
| 1422 | } |
||
| 1591 | holgerb | 1423 | VarioCharacter = '='; |
| 1309 | hbuss | 1424 | } |
| 1425 | // Trim height set point |
||
| 1334 | killagreg | 1426 | if(abs(HeightTrimming) > 512) |
| 1309 | hbuss | 1427 | { |
| 1332 | hbuss | 1428 | SollHoehe += (HeightTrimming * EE_Parameter.Hoehe_Verstaerkung)/(5 * 512 / 2); // move setpoint |
| 1309 | hbuss | 1429 | HeightTrimming = 0; |
| 1587 | killagreg | 1430 | LIMIT_MIN_MAX(SollHoehe, (HoehenWert-1024), (HoehenWert+1024)); // max. 10m Unterschied |
| 1309 | hbuss | 1431 | if(EE_Parameter.ExtraConfig & CFG2_VARIO_BEEP) beeptime = 75; |
| 1320 | hbuss | 1432 | //update hoover gas stick value when setpoint is shifted |
| 1332 | hbuss | 1433 | if(!EE_Parameter.Hoehe_StickNeutralPoint) |
| 1434 | { |
||
| 1587 | killagreg | 1435 | StickGasHover = HoverGas/STICK_GAIN; //rescale back to stick value |
| 1436 | StickGasHover = (StickGasHover * UBat) / BattLowVoltageWarning; |
||
| 1437 | if(StickGasHover < 70) StickGasHover = 70; |
||
| 1438 | else if(StickGasHover > 150) StickGasHover = 150; |
||
| 1332 | hbuss | 1439 | } |
| 1309 | hbuss | 1440 | } |
| 1352 | hbuss | 1441 | if(BaroExpandActive) SollHoehe = HoehenWert; // update setpoint to current altitude if Expanding is active |
| 1420 | killagreg | 1442 | } //if FCFlags & MKFCFLAG_FLY |
| 1330 | killagreg | 1443 | else |
| 1444 | { |
||
| 1322 | hbuss | 1445 | SollHoehe = HoehenWert - 400; |
| 1587 | killagreg | 1446 | if(EE_Parameter.Hoehe_StickNeutralPoint) StickGasHover = EE_Parameter.Hoehe_StickNeutralPoint; |
| 1447 | else StickGasHover = 120; |
||
| 1320 | hbuss | 1448 | } |
| 1590 | killagreg | 1449 | HCGas = HoverGas; // take hover gas (neutral point) |
| 1450 | } |
||
| 1314 | killagreg | 1451 | if(HoehenWert > SollHoehe || !(EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT)) |
| 1283 | hbuss | 1452 | { |
| 1590 | killagreg | 1453 | // from this point the Heigth Control Algorithm is identical for both versions |
| 1454 | if(BaroExpandActive) // baro range expanding active |
||
| 1455 | { |
||
| 1456 | HCGas = HoverGas; // hover while expanding baro adc range |
||
| 1457 | HeightDeviation = 0; |
||
| 1458 | } // EOF // baro range expanding active |
||
| 1459 | else // valid data from air pressure sensor |
||
| 1460 | { |
||
| 1461 | // ------------------------- P-Part ---------------------------- |
||
| 1462 | tmp_long = (HoehenWert - SollHoehe); // positive when too high |
||
| 1463 | LIMIT_MIN_MAX(tmp_long, -32767L, 32767L); // avoid overflov when casting to int16_t |
||
| 1464 | HeightDeviation = (int)(tmp_long); // positive when too high |
||
| 1465 | tmp_long = (tmp_long * (long)Parameter_Hoehe_P) / 16L; // p-part |
||
| 1466 | LIMIT_MIN_MAX(tmp_long, -255 * STICK_GAIN, 255 * STICK_GAIN); // more than 2 times the full range makes no sense |
||
| 1467 | HCGas -= tmp_long; |
||
| 1468 | // ------------------------- D-Part 1: Vario Meter ---------------------------- |
||
| 1469 | tmp_int = VarioMeter / 8; |
||
| 1470 | LIMIT_MIN_MAX(tmp_int, -181, 181); // avoid overflow when squared (181^2 = 32761) |
||
| 1471 | tmp_int2 = tmp_int; |
||
| 1472 | LIMIT_MAX(tmp_int2, 8); // limit quadratic part on upward movement to avoid to much gas reduction |
||
| 1473 | if(tmp_int2 > 0) tmp_int = tmp_int + (tmp_int2 * tmp_int2) / 4; |
||
| 1474 | else tmp_int = tmp_int - (tmp_int2 * tmp_int2) / 4; |
||
| 1475 | tmp_int = (tmp_int * (long)Parameter_Luftdruck_D) / 128L; // scale to d-gain parameter |
||
| 1476 | LIMIT_MIN_MAX(tmp_int,-32 * STICK_GAIN, 64 * STICK_GAIN); |
||
| 1477 | HCGas -= tmp_int; |
||
| 1478 | } // EOF no baro range expanding |
||
| 1309 | hbuss | 1479 | // ------------------------ D-Part 2: ACC-Z Integral ------------------------ |
| 1587 | killagreg | 1480 | tmp_long = ((Mess_Integral_Hoch / 128L) * (int32_t) Parameter_Hoehe_ACC_Wirkung) / (128L / STICK_GAIN); |
| 1481 | LIMIT_MIN_MAX(tmp_long, -32 * STICK_GAIN, 64 * STICK_GAIN); |
||
| 1482 | HCGas -= tmp_long; |
||
| 1483 | // ------------------------ D-Part 3: GpsZ ---------------------------------- |
||
| 1588 | killagreg | 1484 | tmp_int = (Parameter_Hoehe_GPS_Z * (int)FromNaviCtrl_Value.GpsZ)/128L; |
| 1485 | LIMIT_MIN_MAX(tmp_int, -32 * STICK_GAIN, 64 * STICK_GAIN); |
||
| 1309 | hbuss | 1486 | HCGas -= tmp_int; |
| 1587 | killagreg | 1487 | |
| 1309 | hbuss | 1488 | // limit deviation from hoover point within the target region |
| 1587 | killagreg | 1489 | if( (abs(HeightDeviation) < 150) && (!HeightTrimming) && (HoverGas > 0)) // height setpoint is not changed and hoover gas not zero |
| 1309 | hbuss | 1490 | { |
| 1587 | killagreg | 1491 | LIMIT_MIN_MAX(HCGas, HoverGasMin, HoverGasMax); // limit gas around the hoover point |
| 1309 | hbuss | 1492 | } |
| 1276 | hbuss | 1493 | |
| 1322 | hbuss | 1494 | // strech control output by inverse attitude projection 1/cos |
| 1495 | // + 1/cos(angle) ++++++++++++++++++++++++++ |
||
| 1330 | killagreg | 1496 | tmp_long2 = (int32_t)HCGas; |
| 1497 | tmp_long2 *= 8192L; |
||
| 1498 | tmp_long2 /= CosAttitude; |
||
| 1499 | HCGas = (int16_t)tmp_long2; |
||
| 1309 | hbuss | 1500 | // update height control gas averaging |
| 1501 | FilterHCGas = (FilterHCGas * (HC_GAS_AVERAGE - 1) + HCGas) / HC_GAS_AVERAGE; |
||
| 1502 | // limit height control gas pd-control output |
||
| 1503 | LIMIT_MIN_MAX(FilterHCGas, EE_Parameter.Hoehe_MinGas * STICK_GAIN, (MAX_GAS - 20) * STICK_GAIN); |
||
| 1504 | // set GasMischanteil to HeightControlGasFilter |
||
| 1314 | killagreg | 1505 | if(EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT) |
| 1587 | killagreg | 1506 | { // old version |
| 1507 | LIMIT_MAX(FilterHCGas, GasMischanteil); // nicht mehr als Gas |
||
| 1508 | } |
||
| 1309 | hbuss | 1509 | GasMischanteil = FilterHCGas; |
| 1314 | killagreg | 1510 | } |
| 1309 | hbuss | 1511 | }// EOF height control active |
| 1320 | hbuss | 1512 | else // HC not active |
| 1513 | { |
||
| 1514 | //update hoover gas stick value when HC is not active |
||
| 1587 | killagreg | 1515 | if(!EE_Parameter.Hoehe_StickNeutralPoint) |
| 1516 | { |
||
| 1517 | StickGasHover = HoverGas/STICK_GAIN; // rescale back to stick value |
||
| 1518 | StickGasHover = (StickGasHover * UBat) / BattLowVoltageWarning; |
||
| 1322 | hbuss | 1519 | } |
| 1587 | killagreg | 1520 | else StickGasHover = EE_Parameter.Hoehe_StickNeutralPoint; |
| 1521 | LIMIT_MIN_MAX(StickGasHover, 70, 150); // reserve some range for trim up and down |
||
| 1328 | hbuss | 1522 | FilterHCGas = GasMischanteil; |
| 1330 | killagreg | 1523 | } |
| 1283 | hbuss | 1524 | |
| 1587 | killagreg | 1525 | // Hover gas estimation by averaging gas control output on small z-velocities |
| 1309 | hbuss | 1526 | // this is done only if height contol option is selected in global config and aircraft is flying |
| 1420 | killagreg | 1527 | if((FCFlags & FCFLAG_FLY) && !(FCFlags & FCFLAG_NOTLANDUNG)) |
| 1309 | hbuss | 1528 | { |
| 1590 | killagreg | 1529 | if(HoverGasFilter == 0) HoverGasFilter = HOVER_GAS_AVERAGE * (unsigned long)(GasMischanteil); // init estimation |
| 1309 | hbuss | 1530 | if(abs(VarioMeter) < 100) // only on small vertical speed |
| 1531 | { |
||
| 1330 | killagreg | 1532 | tmp_long2 = (int32_t)GasMischanteil; // take current thrust |
| 1533 | tmp_long2 *= CosAttitude; // apply attitude projection |
||
| 1534 | tmp_long2 /= 8192; |
||
| 1535 | |||
| 1309 | hbuss | 1536 | // average vertical projected thrust |
| 1537 | if(modell_fliegt < 2000) // the first 4 seconds |
||
| 1538 | { // reduce the time constant of averaging by factor of 8 to get much faster a stable value |
||
| 1590 | killagreg | 1539 | HoverGasFilter -= HoverGasFilter/(HOVER_GAS_AVERAGE/8L); |
| 1587 | killagreg | 1540 | HoverGasFilter += 8L * tmp_long2; |
| 1309 | hbuss | 1541 | } |
| 1542 | else if(modell_fliegt < 4000) // the first 8 seconds |
||
| 1543 | { // reduce the time constant of averaging by factor of 4 to get much faster a stable value |
||
| 1590 | killagreg | 1544 | HoverGasFilter -= HoverGasFilter/(HOVER_GAS_AVERAGE/4L); |
| 1587 | killagreg | 1545 | HoverGasFilter += 4L * tmp_long2; |
| 1309 | hbuss | 1546 | } |
| 1547 | else if(modell_fliegt < 8000) // the first 16 seconds |
||
| 1548 | { // reduce the time constant of averaging by factor of 2 to get much faster a stable value |
||
| 1590 | killagreg | 1549 | HoverGasFilter -= HoverGasFilter/(HOVER_GAS_AVERAGE/2L); |
| 1587 | killagreg | 1550 | HoverGasFilter += 2L * tmp_long2; |
| 1309 | hbuss | 1551 | } |
| 1552 | else //later |
||
| 1553 | { |
||
| 1590 | killagreg | 1554 | HoverGasFilter -= HoverGasFilter/HOVER_GAS_AVERAGE; |
| 1587 | killagreg | 1555 | HoverGasFilter += tmp_long2; |
| 1309 | hbuss | 1556 | } |
| 1590 | killagreg | 1557 | HoverGas = (int16_t)(HoverGasFilter/HOVER_GAS_AVERAGE); |
| 1309 | hbuss | 1558 | if(EE_Parameter.Hoehe_HoverBand) |
| 1559 | { |
||
| 1560 | int16_t band; |
||
| 1587 | killagreg | 1561 | band = HoverGas / EE_Parameter.Hoehe_HoverBand; // the higher the parameter the smaller the range |
| 1562 | HoverGasMin = HoverGas - band; |
||
| 1563 | HoverGasMax = HoverGas + band; |
||
| 1309 | hbuss | 1564 | } |
| 1565 | else |
||
| 1566 | { // no limit |
||
| 1587 | killagreg | 1567 | HoverGasMin = 0; |
| 1568 | HoverGasMax = 1023; |
||
| 1309 | hbuss | 1569 | } |
| 1570 | } |
||
| 1571 | } |
||
| 1572 | }// EOF ParamSet.GlobalConfig & CFG_HEIGHT_CONTROL |
||
| 1573 | |||
| 1574 | // limit gas to parameter setting |
||
| 1320 | hbuss | 1575 | LIMIT_MIN(GasMischanteil, (MIN_GAS + 10) * STICK_GAIN); |
| 855 | hbuss | 1576 | if(GasMischanteil > (MAX_GAS - 20) * STICK_GAIN) GasMischanteil = (MAX_GAS - 20) * STICK_GAIN; |
| 1111 | hbuss | 1577 | |
| 1051 | killagreg | 1578 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1320 | hbuss | 1579 | // all BL-Ctrl connected? |
| 1580 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1330 | killagreg | 1581 | if(MissingMotor) |
| 1320 | hbuss | 1582 | if(modell_fliegt > 1 && modell_fliegt < 50 && GasMischanteil > 0) |
| 1583 | { |
||
| 1584 | modell_fliegt = 1; |
||
| 1585 | GasMischanteil = MIN_GAS; |
||
| 1586 | } |
||
| 1587 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1 | ingob | 1588 | // + Mischer und PI-Regler |
| 1051 | killagreg | 1589 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 173 | holgerb | 1590 | DebugOut.Analog[7] = GasMischanteil; |
| 1051 | killagreg | 1591 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 1592 | // Gier-Anteil |
| 1051 | killagreg | 1593 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 855 | hbuss | 1594 | GierMischanteil = MesswertGier - sollGier * STICK_GAIN; // Regler für Gier |
| 1595 | #define MIN_GIERGAS (40*STICK_GAIN) // unter diesem Gaswert trotzdem Gieren |
||
| 693 | hbuss | 1596 | if(GasMischanteil > MIN_GIERGAS) |
| 1597 | { |
||
| 1051 | killagreg | 1598 | if(GierMischanteil > (GasMischanteil / 2)) GierMischanteil = GasMischanteil / 2; |
| 1599 | if(GierMischanteil < -(GasMischanteil / 2)) GierMischanteil = -(GasMischanteil / 2); |
||
| 693 | hbuss | 1600 | } |
| 1051 | killagreg | 1601 | else |
| 693 | hbuss | 1602 | { |
| 1051 | killagreg | 1603 | if(GierMischanteil > (MIN_GIERGAS / 2)) GierMischanteil = MIN_GIERGAS / 2; |
| 1604 | if(GierMischanteil < -(MIN_GIERGAS / 2)) GierMischanteil = -(MIN_GIERGAS / 2); |
||
| 693 | hbuss | 1605 | } |
| 855 | hbuss | 1606 | tmp_int = MAX_GAS*STICK_GAIN; |
| 1051 | killagreg | 1607 | if(GierMischanteil > ((tmp_int - GasMischanteil))) GierMischanteil = ((tmp_int - GasMischanteil)); |
| 855 | hbuss | 1608 | if(GierMischanteil < -((tmp_int - GasMischanteil))) GierMischanteil = -((tmp_int - GasMischanteil)); |
| 513 | hbuss | 1609 | |
| 1051 | killagreg | 1610 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 1611 | // Nick-Achse |
| 1051 | killagreg | 1612 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 723 | hbuss | 1613 | DiffNick = MesswertNick - StickNick; // Differenz bestimmen |
| 1153 | hbuss | 1614 | if(IntegralFaktor) SummeNick += IntegralNickMalFaktor - StickNick; // I-Anteil bei Winkelregelung |
| 1051 | killagreg | 1615 | else SummeNick += DiffNick; // I-Anteil bei HH |
| 855 | hbuss | 1616 | if(SummeNick > (STICK_GAIN * 16000L)) SummeNick = (STICK_GAIN * 16000L); |
| 1617 | if(SummeNick < -(16000L * STICK_GAIN)) SummeNick = -(16000L * STICK_GAIN); |
||
| 1153 | hbuss | 1618 | pd_ergebnis_nick = DiffNick + SummeNick / Ki; // PI-Regler für Nick |
| 1 | ingob | 1619 | // Motor Vorn |
| 499 | hbuss | 1620 | tmp_int = (long)((long)Parameter_DynamicStability * (long)(GasMischanteil + abs(GierMischanteil)/2)) / 64; |
| 1153 | hbuss | 1621 | if(pd_ergebnis_nick > tmp_int) pd_ergebnis_nick = tmp_int; |
| 1622 | if(pd_ergebnis_nick < -tmp_int) pd_ergebnis_nick = -tmp_int; |
||
| 173 | holgerb | 1623 | |
| 1153 | hbuss | 1624 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1625 | // Roll-Achse |
||
| 1626 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1627 | DiffRoll = MesswertRoll - StickRoll; // Differenz bestimmen |
||
| 1628 | if(IntegralFaktor) SummeRoll += IntegralRollMalFaktor - StickRoll;// I-Anteil bei Winkelregelung |
||
| 1629 | else SummeRoll += DiffRoll; // I-Anteil bei HH |
||
| 1630 | if(SummeRoll > (STICK_GAIN * 16000L)) SummeRoll = (STICK_GAIN * 16000L); |
||
| 1631 | if(SummeRoll < -(16000L * STICK_GAIN)) SummeRoll = -(16000L * STICK_GAIN); |
||
| 1632 | pd_ergebnis_roll = DiffRoll + SummeRoll / Ki; // PI-Regler für Roll |
||
| 1633 | tmp_int = (long)((long)Parameter_DynamicStability * (long)(GasMischanteil + abs(GierMischanteil)/2)) / 64; |
||
| 1634 | if(pd_ergebnis_roll > tmp_int) pd_ergebnis_roll = tmp_int; |
||
| 1635 | if(pd_ergebnis_roll < -tmp_int) pd_ergebnis_roll = -tmp_int; |
||
| 1636 | |||
| 1637 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1209 | hbuss | 1638 | // Universal Mixer |
| 1155 | hbuss | 1639 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1642 | killagreg | 1640 | for(i=0; i<MAX_MOTORS; i++) |
| 1641 | { |
||
| 1642 | signed int tmp_int; |
||
| 1643 | if(Mixer.Motor[i][0] > 0) |
||
| 1644 | { |
||
| 1645 | tmp_int = ((long)GasMischanteil * Mixer.Motor[i][0]) / 64L; |
||
| 1646 | tmp_int += ((long)pd_ergebnis_nick * Mixer.Motor[i][1]) / 64L; |
||
| 1647 | tmp_int += ((long)pd_ergebnis_roll * Mixer.Motor[i][2]) / 64L; |
||
| 1648 | tmp_int += ((long)GierMischanteil * Mixer.Motor[i][3]) / 64L; |
||
| 1649 | tmp_motorwert[i] = MotorSmoothing(tmp_int,tmp_motorwert[i]); // Filter |
||
| 1650 | tmp_int = tmp_motorwert[i] / 4; |
||
| 1651 | Motor[i].SetPointLowerBits = tmp_motorwert[i] % 4; |
||
| 1652 | LIMIT_MIN_MAX(tmp_int,MIN_GAS,MAX_GAS); |
||
| 1653 | Motor[i].SetPoint = tmp_int; |
||
| 1654 | } |
||
| 1655 | else |
||
| 1656 | { |
||
| 1657 | Motor[i].SetPoint = 0; |
||
| 1658 | Motor[i].SetPointLowerBits = 0; |
||
| 1659 | } |
||
| 1660 | } |
||
| 1111 | hbuss | 1661 | } |