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| Rev | Author | Line No. | Line |
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| 1 | ingob | 1 | /*####################################################################################### |
| 2 | Flight Control |
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| 3 | #######################################################################################*/ |
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| 4 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
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| 5 | // + Copyright (c) 04.2007 Holger Buss |
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| 6 | // + Nur für den privaten Gebrauch |
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| 7 | // + www.MikroKopter.com |
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| 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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| 1051 | killagreg | 27 | // + Die Portierung 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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| 831 | hbuss | 42 | // + * porting to systems other than 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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| 492 | hbuss | 50 | // + INTERRUPTION) HOWEVER CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN// + CONTRACT, STRICT LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) |
| 1 | ingob | 51 | // + ARISING IN ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE |
| 1051 | killagreg | 52 | // + POSSIBILITY OF SUCH DAMAGE. |
| 1 | ingob | 53 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 54 | |||
| 55 | #include "main.h" |
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| 395 | hbuss | 56 | #include "eeprom.c" |
| 1 | ingob | 57 | |
| 58 | unsigned char h,m,s; |
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| 173 | holgerb | 59 | volatile unsigned int I2CTimeout = 100; |
| 1153 | hbuss | 60 | int MesswertNick,MesswertRoll,MesswertGier,MesswertGierBias, RohMesswertNick,RohMesswertRoll; |
| 1166 | hbuss | 61 | int TrimNick, TrimRoll; |
| 1051 | killagreg | 62 | int AdNeutralGierBias; |
| 927 | hbuss | 63 | int AdNeutralNick = 0,AdNeutralRoll = 0,AdNeutralGier = 0,StartNeutralRoll = 0,StartNeutralNick = 0; |
| 64 | int Mittelwert_AccNick, Mittelwert_AccRoll,Mittelwert_AccHoch, NeutralAccX=0, NeutralAccY=0; |
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| 805 | hbuss | 65 | int NaviAccNick, NaviAccRoll,NaviCntAcc = 0; |
| 1 | ingob | 66 | volatile float NeutralAccZ = 0; |
| 67 | unsigned char CosinusNickWinkel = 0, CosinusRollWinkel = 0; |
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| 693 | hbuss | 68 | long IntegralNick = 0,IntegralNick2 = 0; |
| 69 | long IntegralRoll = 0,IntegralRoll2 = 0; |
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| 70 | long IntegralAccNick = 0,IntegralAccRoll = 0,IntegralAccZ = 0; |
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| 71 | long Integral_Gier = 0; |
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| 72 | long Mess_IntegralNick = 0,Mess_IntegralNick2 = 0; |
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| 73 | long Mess_IntegralRoll = 0,Mess_IntegralRoll2 = 0; |
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| 74 | long Mess_Integral_Gier = 0,Mess_Integral_Gier2 = 0; |
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| 75 | long MittelIntegralNick,MittelIntegralRoll,MittelIntegralNick2,MittelIntegralRoll2; |
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| 1 | ingob | 76 | volatile long Mess_Integral_Hoch = 0; |
| 1153 | hbuss | 77 | int KompassValue = 0; |
| 78 | int KompassStartwert = 0; |
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| 79 | int KompassRichtung = 0; |
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| 693 | hbuss | 80 | unsigned int KompassSignalSchlecht = 500; |
| 855 | hbuss | 81 | unsigned char MAX_GAS,MIN_GAS; |
| 1 | ingob | 82 | unsigned char Notlandung = 0; |
| 83 | unsigned char HoehenReglerAktiv = 0; |
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| 880 | hbuss | 84 | unsigned char TrichterFlug = 0; |
| 395 | hbuss | 85 | long Umschlag180Nick = 250000L, Umschlag180Roll = 250000L; |
| 693 | hbuss | 86 | long ErsatzKompass; |
| 87 | int ErsatzKompassInGrad; // Kompasswert in Grad |
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| 88 | int GierGyroFehler = 0; |
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| 1153 | hbuss | 89 | char GyroFaktor; |
| 90 | char IntegralFaktor; |
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| 91 | int DiffNick,DiffRoll; |
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| 1051 | killagreg | 92 | int Poti1 = 0, Poti2 = 0, Poti3 = 0, Poti4 = 0; |
| 1166 | hbuss | 93 | volatile unsigned char Motor_Vorne,Motor_Hinten,Motor_Rechts,Motor_Links; |
| 1111 | hbuss | 94 | volatile unsigned char Motor1, Motor2,Motor3,Motor4,Motor5,Motor6,Motor7,Motor8; |
| 1 | ingob | 95 | volatile unsigned char SenderOkay = 0; |
| 595 | hbuss | 96 | int StickNick = 0,StickRoll = 0,StickGier = 0,StickGas = 0; |
| 1 | ingob | 97 | char MotorenEin = 0; |
| 98 | int HoehenWert = 0; |
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| 99 | int SollHoehe = 0; |
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| 498 | hbuss | 100 | int LageKorrekturRoll = 0,LageKorrekturNick = 0; |
| 1153 | hbuss | 101 | //float Ki = FAKTOR_I; |
| 102 | int Ki = 10300 / 33; |
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| 395 | hbuss | 103 | unsigned char Looping_Nick = 0,Looping_Roll = 0; |
| 104 | unsigned char Looping_Links = 0, Looping_Rechts = 0, Looping_Unten = 0, Looping_Oben = 0; |
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| 1 | ingob | 105 | |
| 106 | unsigned char Parameter_Luftdruck_D = 48; // Wert : 0-250 |
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| 107 | unsigned char Parameter_MaxHoehe = 251; // Wert : 0-250 |
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| 108 | unsigned char Parameter_Hoehe_P = 16; // Wert : 0-32 |
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| 109 | unsigned char Parameter_Hoehe_ACC_Wirkung = 58; // Wert : 0-250 |
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| 110 | unsigned char Parameter_KompassWirkung = 64; // Wert : 0-250 |
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| 1111 | hbuss | 111 | unsigned char Parameter_Gyro_D = 8; // Wert : 0-250 |
| 173 | holgerb | 112 | unsigned char Parameter_Gyro_P = 150; // Wert : 10-250 |
| 1 | ingob | 113 | unsigned char Parameter_Gyro_I = 150; // Wert : 0-250 |
| 114 | unsigned char Parameter_Gier_P = 2; // Wert : 1-20 |
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| 115 | unsigned char Parameter_I_Faktor = 10; // Wert : 1-20 |
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| 116 | unsigned char Parameter_UserParam1 = 0; |
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| 117 | unsigned char Parameter_UserParam2 = 0; |
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| 118 | unsigned char Parameter_UserParam3 = 0; |
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| 119 | unsigned char Parameter_UserParam4 = 0; |
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| 499 | hbuss | 120 | unsigned char Parameter_UserParam5 = 0; |
| 121 | unsigned char Parameter_UserParam6 = 0; |
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| 122 | unsigned char Parameter_UserParam7 = 0; |
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| 123 | unsigned char Parameter_UserParam8 = 0; |
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| 1 | ingob | 124 | unsigned char Parameter_ServoNickControl = 100; |
| 173 | holgerb | 125 | unsigned char Parameter_LoopGasLimit = 70; |
| 1120 | hbuss | 126 | unsigned char Parameter_AchsKopplung1 = 90; |
| 127 | unsigned char Parameter_AchsKopplung2 = 65; |
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| 128 | unsigned char Parameter_CouplingYawCorrection = 64; |
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| 129 | //unsigned char Parameter_AchsGegenKopplung1 = 0; |
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| 499 | hbuss | 130 | unsigned char Parameter_DynamicStability = 100; |
| 921 | hbuss | 131 | unsigned char Parameter_J16Bitmask; // for the J16 Output |
| 132 | unsigned char Parameter_J16Timing; // for the J16 Output |
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| 133 | unsigned char Parameter_J17Bitmask; // for the J17 Output |
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| 134 | unsigned char Parameter_J17Timing; // for the J17 Output |
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| 135 | unsigned char Parameter_NaviGpsModeControl; // Parameters for the Naviboard |
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| 1051 | killagreg | 136 | unsigned char Parameter_NaviGpsGain; |
| 137 | unsigned char Parameter_NaviGpsP; |
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| 138 | unsigned char Parameter_NaviGpsI; |
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| 139 | unsigned char Parameter_NaviGpsD; |
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| 140 | unsigned char Parameter_NaviGpsACC; |
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| 993 | hbuss | 141 | unsigned char Parameter_NaviOperatingRadius; |
| 142 | unsigned char Parameter_NaviWindCorrection; |
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| 143 | unsigned char Parameter_NaviSpeedCompensation; |
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| 921 | hbuss | 144 | unsigned char Parameter_ExternalControl; |
| 1 | ingob | 145 | struct mk_param_struct EE_Parameter; |
| 492 | hbuss | 146 | signed int ExternStickNick = 0,ExternStickRoll = 0,ExternStickGier = 0, ExternHoehenValue = -20; |
| 614 | hbuss | 147 | int MaxStickNick = 0,MaxStickRoll = 0; |
| 871 | hbuss | 148 | unsigned int modell_fliegt = 0; |
| 1209 | hbuss | 149 | volatile unsigned char MikroKopterFlags = 0; |
| 1121 | hbuss | 150 | long GIER_GRAD_FAKTOR = 1291; |
| 1153 | hbuss | 151 | signed int KopplungsteilNickRoll,KopplungsteilRollNick; |
| 1209 | hbuss | 152 | unsigned char RequiredMotors = 4; |
| 1 | ingob | 153 | |
| 1209 | hbuss | 154 | /* |
| 155 | signed char Mixer.Motor[MAX_MOTORS][4] = { |
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| 156 | {64, +64, 0, +64},//1 |
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| 157 | {64, +64, -64, -64},//2 |
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| 158 | {64, 0, -64, +64},//3 |
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| 159 | {64, -64, -64, -64},//4 |
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| 160 | {64, -64, 0, +64},//5 |
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| 161 | {64, -64, +64, -64},//6 |
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| 162 | {64, 0, +64, +64},//7 |
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| 163 | {64, +64, +64, -64},//8 |
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| 164 | { 0, 0, 0, 0},//9 |
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| 165 | { 0, 0, 0, 0},//10 |
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| 166 | { 0, 0, 0, 0},//11 |
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| 167 | { 0, 0, 0, 0}};//12 |
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| 168 | */ |
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| 169 | /* |
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| 170 | signed char Mixer.Motor[MAX_MOTORS][4] = { |
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| 171 | { 64, +64, 0, +64},//1 |
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| 172 | { 64, -64, 0, +64},//2 |
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| 173 | { 64, 0, -64, -64},//3 |
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| 174 | { 64, 0, +64, -64},//4 |
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| 175 | { 0, 0, 0, 0},//5 |
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| 176 | { 0, 0, 0, 0},//6 |
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| 177 | { 0, 0, 0, 0},//7 |
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| 178 | { 0, 0, 0, 0},//8 |
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| 179 | { 0, 0, 0, 0},//9 |
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| 180 | { 0, 0, 0, 0},//10 |
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| 181 | { 0, 0, 0, 0},//11 |
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| 182 | { 0, 0, 0, 0}};//12 |
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| 183 | */ |
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| 184 | unsigned char Motor[MAX_MOTORS]; |
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| 185 | signed int tmp_motorwert[MAX_MOTORS]; |
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| 1155 | hbuss | 186 | |
| 1166 | hbuss | 187 | int MotorSmoothing(int neu, int alt) |
| 188 | { |
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| 189 | int motor; |
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| 190 | if(neu > alt) motor = (1*(int)alt + neu) / 2; |
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| 191 | else motor = neu - (alt - neu)*1; |
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| 192 | //if(Poti2 < 20) return(neu); |
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| 193 | return(motor); |
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| 194 | } |
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| 195 | |||
| 196 | |||
| 1 | ingob | 197 | void Piep(unsigned char Anzahl) |
| 198 | { |
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| 199 | while(Anzahl--) |
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| 200 | { |
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| 201 | if(MotorenEin) return; //auf keinen Fall im Flug! |
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| 202 | beeptime = 100; |
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| 203 | Delay_ms(250); |
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| 204 | } |
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| 205 | } |
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| 206 | |||
| 207 | //############################################################################ |
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| 208 | // Nullwerte ermitteln |
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| 209 | void SetNeutral(void) |
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| 210 | //############################################################################ |
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| 211 | { |
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| 1111 | hbuss | 212 | unsigned char i; |
| 213 | unsigned int gier_neutral=0, nick_neutral=0, roll_neutral=0; |
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| 1171 | hbuss | 214 | ServoActive = 0; HEF4017R_ON; |
| 1051 | killagreg | 215 | NeutralAccX = 0; |
| 1 | ingob | 216 | NeutralAccY = 0; |
| 217 | NeutralAccZ = 0; |
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| 1051 | killagreg | 218 | AdNeutralNick = 0; |
| 219 | AdNeutralRoll = 0; |
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| 1 | ingob | 220 | AdNeutralGier = 0; |
| 927 | hbuss | 221 | AdNeutralGierBias = 0; |
| 395 | hbuss | 222 | Parameter_AchsKopplung1 = 0; |
| 1120 | hbuss | 223 | Parameter_AchsKopplung2 = 0; |
| 1036 | hbuss | 224 | ExpandBaro = 0; |
| 1051 | killagreg | 225 | CalibrierMittelwert(); |
| 395 | hbuss | 226 | Delay_ms_Mess(100); |
| 1 | ingob | 227 | CalibrierMittelwert(); |
| 228 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG)) // Höhenregelung aktiviert? |
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| 1051 | killagreg | 229 | { |
| 1 | ingob | 230 | if((MessLuftdruck > 950) || (MessLuftdruck < 750)) SucheLuftruckOffset(); |
| 231 | } |
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| 1166 | hbuss | 232 | #define NEUTRAL_FILTER 32 |
| 233 | for(i=0; i<NEUTRAL_FILTER; i++) |
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| 1111 | hbuss | 234 | { |
| 235 | Delay_ms_Mess(10); |
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| 236 | gier_neutral += AdWertGier; |
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| 1166 | hbuss | 237 | nick_neutral += AdWertNick; |
| 238 | roll_neutral += AdWertRoll; |
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| 1111 | hbuss | 239 | } |
| 1173 | hbuss | 240 | AdNeutralNick= (nick_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER / 8); |
| 241 | AdNeutralRoll= (roll_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER / 8); |
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| 242 | AdNeutralGier= (gier_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER); |
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| 1111 | hbuss | 243 | AdNeutralGierBias = AdNeutralGier; |
| 401 | hbuss | 244 | StartNeutralRoll = AdNeutralRoll; |
| 245 | StartNeutralNick = AdNeutralNick; |
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| 1051 | killagreg | 246 | if(eeprom_read_byte(&EEPromArray[EEPROM_ADR_ACC_NICK]) > 4) |
| 513 | hbuss | 247 | { |
| 1171 | hbuss | 248 | NeutralAccY = abs(Mittelwert_AccRoll) / (2*ACC_AMPLIFY); |
| 249 | NeutralAccX = abs(Mittelwert_AccNick) / (2*ACC_AMPLIFY); |
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| 513 | hbuss | 250 | NeutralAccZ = Aktuell_az; |
| 251 | } |
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| 1051 | killagreg | 252 | else |
| 513 | hbuss | 253 | { |
| 254 | NeutralAccX = (int)eeprom_read_byte(&EEPromArray[EEPROM_ADR_ACC_NICK]) * 256 + (int)eeprom_read_byte(&EEPromArray[EEPROM_ADR_ACC_NICK+1]); |
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| 255 | NeutralAccY = (int)eeprom_read_byte(&EEPromArray[EEPROM_ADR_ACC_ROLL]) * 256 + (int)eeprom_read_byte(&EEPromArray[EEPROM_ADR_ACC_ROLL+1]); |
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| 256 | NeutralAccZ = (int)eeprom_read_byte(&EEPromArray[EEPROM_ADR_ACC_Z]) * 256 + (int)eeprom_read_byte(&EEPromArray[EEPROM_ADR_ACC_Z+1]); |
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| 257 | } |
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| 1051 | killagreg | 258 | |
| 1 | ingob | 259 | MesswertNick = 0; |
| 260 | MesswertRoll = 0; |
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| 261 | MesswertGier = 0; |
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| 1111 | hbuss | 262 | Delay_ms_Mess(100); |
| 1174 | hbuss | 263 | Mittelwert_AccNick = ACC_AMPLIFY * (long)AdWertAccNick; |
| 264 | Mittelwert_AccRoll = ACC_AMPLIFY * (long)AdWertAccRoll; |
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| 1173 | hbuss | 265 | IntegralNick = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccNick; |
| 266 | IntegralRoll = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccRoll; |
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| 267 | Mess_IntegralNick2 = IntegralNick; |
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| 268 | Mess_IntegralRoll2 = IntegralRoll; |
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| 269 | Mess_Integral_Gier = 0; |
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| 1 | ingob | 270 | StartLuftdruck = Luftdruck; |
| 271 | HoeheD = 0; |
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| 272 | Mess_Integral_Hoch = 0; |
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| 273 | KompassStartwert = KompassValue; |
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| 274 | GPS_Neutral(); |
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| 1051 | killagreg | 275 | beeptime = 50; |
| 882 | hbuss | 276 | Umschlag180Nick = ((long) EE_Parameter.WinkelUmschlagNick * 2500L) + 15000L; |
| 277 | Umschlag180Roll = ((long) EE_Parameter.WinkelUmschlagRoll * 2500L) + 15000L; |
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| 492 | hbuss | 278 | ExternHoehenValue = 0; |
| 693 | hbuss | 279 | ErsatzKompass = KompassValue * GIER_GRAD_FAKTOR; |
| 280 | GierGyroFehler = 0; |
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| 723 | hbuss | 281 | SendVersionToNavi = 1; |
| 921 | hbuss | 282 | LED_Init(); |
| 283 | MikroKopterFlags |= FLAG_CALIBRATE; |
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| 992 | hbuss | 284 | FromNaviCtrl_Value.Kalman_K = -1; |
| 1173 | hbuss | 285 | FromNaviCtrl_Value.Kalman_MaxDrift = 0; |
| 992 | hbuss | 286 | FromNaviCtrl_Value.Kalman_MaxFusion = 32; |
| 1172 | hbuss | 287 | Poti1 = PPM_in[EE_Parameter.Kanalbelegung[K_POTI1]] + 110; |
| 288 | Poti2 = PPM_in[EE_Parameter.Kanalbelegung[K_POTI2]] + 110; |
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| 289 | Poti3 = PPM_in[EE_Parameter.Kanalbelegung[K_POTI3]] + 110; |
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| 290 | Poti4 = PPM_in[EE_Parameter.Kanalbelegung[K_POTI4]] + 110; |
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| 1171 | hbuss | 291 | ServoActive = 1; |
| 292 | SenderOkay = 100; |
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| 1 | ingob | 293 | } |
| 294 | |||
| 295 | //############################################################################ |
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| 395 | hbuss | 296 | // Bearbeitet die Messwerte |
| 1 | ingob | 297 | void Mittelwert(void) |
| 298 | //############################################################################ |
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| 1051 | killagreg | 299 | { |
| 1111 | hbuss | 300 | static signed long tmpl,tmpl2,tmpl3,tmpl4; |
| 301 | static signed int oldNick, oldRoll, d2Roll, d2Nick; |
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| 1153 | hbuss | 302 | signed long winkel_nick, winkel_roll; |
| 1171 | hbuss | 303 | |
| 1111 | hbuss | 304 | MesswertGier = (signed int) AdNeutralGier - AdWertGier; |
| 305 | // MesswertGierBias = (signed int) AdNeutralGierBias - AdWertGier; |
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| 1171 | hbuss | 306 | MesswertNick = (signed int) AdWertNickFilter / 8; |
| 307 | MesswertRoll = (signed int) AdWertRollFilter / 8; |
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| 1153 | hbuss | 308 | RohMesswertNick = MesswertNick; |
| 309 | RohMesswertRoll = MesswertRoll; |
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| 1120 | hbuss | 310 | //DebugOut.Analog[21] = MesswertNick; |
| 311 | //DebugOut.Analog[22] = MesswertRoll; |
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| 1121 | hbuss | 312 | //DebugOut.Analog[22] = Mess_Integral_Gier; |
| 1166 | hbuss | 313 | //DebugOut.Analog[21] = MesswertNick; |
| 314 | //DebugOut.Analog[22] = MesswertRoll; |
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| 315 | |||
| 395 | hbuss | 316 | // Beschleunigungssensor ++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1166 | hbuss | 317 | Mittelwert_AccNick = ((long)Mittelwert_AccNick * 3 + ((ACC_AMPLIFY * (long)AdWertAccNick))) / 4L; |
| 318 | Mittelwert_AccRoll = ((long)Mittelwert_AccRoll * 3 + ((ACC_AMPLIFY * (long)AdWertAccRoll))) / 4L; |
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| 319 | Mittelwert_AccHoch = ((long)Mittelwert_AccHoch * 3 + ((long)AdWertAccHoch)) / 4L; |
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| 395 | hbuss | 320 | IntegralAccNick += ACC_AMPLIFY * AdWertAccNick; |
| 321 | IntegralAccRoll += ACC_AMPLIFY * AdWertAccRoll; |
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| 805 | hbuss | 322 | NaviAccNick += AdWertAccNick; |
| 323 | NaviAccRoll += AdWertAccRoll; |
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| 324 | NaviCntAcc++; |
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| 1153 | hbuss | 325 | IntegralAccZ += Aktuell_az - NeutralAccZ; |
| 326 | |||
| 1155 | hbuss | 327 | //++++++++++++++++++++++++++++++++++++++++++++++++ |
| 328 | // ADC einschalten |
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| 1171 | hbuss | 329 | ANALOG_ON; |
| 1155 | hbuss | 330 | AdReady = 0; |
| 331 | //++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 332 | |||
| 1153 | hbuss | 333 | if(Mess_IntegralRoll > 93000L) winkel_roll = 93000L; |
| 334 | else if(Mess_IntegralRoll <-93000L) winkel_roll = -93000L; |
||
| 335 | else winkel_roll = Mess_IntegralRoll; |
||
| 336 | |||
| 337 | if(Mess_IntegralNick > 93000L) winkel_nick = 93000L; |
||
| 338 | else if(Mess_IntegralNick <-93000L) winkel_nick = -93000L; |
||
| 339 | else winkel_nick = Mess_IntegralNick; |
||
| 340 | |||
| 1120 | hbuss | 341 | // Gier ++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1153 | hbuss | 342 | Mess_Integral_Gier += MesswertGier; |
| 343 | ErsatzKompass += MesswertGier; |
||
| 395 | hbuss | 344 | // Kopplungsanteil +++++++++++++++++++++++++++++++++++++ |
| 345 | if(!Looping_Nick && !Looping_Roll && (EE_Parameter.GlobalConfig & CFG_ACHSENKOPPLUNG_AKTIV)) |
||
| 346 | { |
||
| 1153 | hbuss | 347 | tmpl3 = (MesswertRoll * winkel_nick) / 2048L; |
| 1120 | hbuss | 348 | tmpl3 *= Parameter_AchsKopplung2; //65 |
| 1111 | hbuss | 349 | tmpl3 /= 4096L; |
| 1153 | hbuss | 350 | tmpl4 = (MesswertNick * winkel_roll) / 2048L; |
| 1120 | hbuss | 351 | tmpl4 *= Parameter_AchsKopplung2; //65 |
| 1111 | hbuss | 352 | tmpl4 /= 4096L; |
| 1153 | hbuss | 353 | KopplungsteilNickRoll = tmpl3; |
| 354 | KopplungsteilRollNick = tmpl4; |
||
| 1111 | hbuss | 355 | tmpl4 -= tmpl3; |
| 356 | ErsatzKompass += tmpl4; |
||
| 1166 | hbuss | 357 | if(!Parameter_CouplingYawCorrection) Mess_Integral_Gier -= tmpl4/2; // Gier nachhelfen |
| 1111 | hbuss | 358 | |
| 1153 | hbuss | 359 | tmpl = ((MesswertGier + tmpl4) * winkel_nick) / 2048L; |
| 1111 | hbuss | 360 | tmpl *= Parameter_AchsKopplung1; // 90 |
| 880 | hbuss | 361 | tmpl /= 4096L; |
| 1153 | hbuss | 362 | tmpl2 = ((MesswertGier + tmpl4) * winkel_roll) / 2048L; |
| 395 | hbuss | 363 | tmpl2 *= Parameter_AchsKopplung1; |
| 880 | hbuss | 364 | tmpl2 /= 4096L; |
| 1153 | hbuss | 365 | if(labs(tmpl) > 128 || labs(tmpl2) > 128 /* || abs(KopplungsteilNickRoll) > 128 || abs(KopplungsteilRollNick) > 128)*/) TrichterFlug = 1; |
| 366 | //MesswertGier += (Parameter_CouplingYawCorrection * tmpl4) / 256; |
||
| 395 | hbuss | 367 | } |
| 1166 | hbuss | 368 | else tmpl = tmpl2 = KopplungsteilNickRoll = KopplungsteilRollNick = 0; |
| 1111 | hbuss | 369 | |
| 1166 | hbuss | 370 | TrimRoll = tmpl - tmpl2 / 100L; |
| 371 | TrimNick = -tmpl2 + tmpl / 100L; |
||
| 372 | |||
| 1111 | hbuss | 373 | // Kompasswert begrenzen ++++++++++++++++++++++++++++++++++++++++++++++++ |
| 374 | if(ErsatzKompass >= (360L * GIER_GRAD_FAKTOR)) ErsatzKompass -= 360L * GIER_GRAD_FAKTOR; // 360° Umschlag |
||
| 375 | if(ErsatzKompass < 0) ErsatzKompass += 360L * GIER_GRAD_FAKTOR; |
||
| 395 | hbuss | 376 | // Roll ++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1166 | hbuss | 377 | Mess_IntegralRoll2 += MesswertRoll + TrimRoll; |
| 378 | Mess_IntegralRoll += MesswertRoll + TrimRoll - LageKorrekturRoll; |
||
| 1051 | killagreg | 379 | if(Mess_IntegralRoll > Umschlag180Roll) |
| 395 | hbuss | 380 | { |
| 882 | hbuss | 381 | Mess_IntegralRoll = -(Umschlag180Roll - 25000L); |
| 395 | hbuss | 382 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
| 1051 | killagreg | 383 | } |
| 395 | hbuss | 384 | if(Mess_IntegralRoll <-Umschlag180Roll) |
| 385 | { |
||
| 882 | hbuss | 386 | Mess_IntegralRoll = (Umschlag180Roll - 25000L); |
| 395 | hbuss | 387 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
| 1051 | killagreg | 388 | } |
| 395 | hbuss | 389 | // Nick ++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1166 | hbuss | 390 | Mess_IntegralNick2 += MesswertNick + TrimNick; |
| 391 | Mess_IntegralNick += MesswertNick + TrimNick - LageKorrekturNick; |
||
| 1051 | killagreg | 392 | if(Mess_IntegralNick > Umschlag180Nick) |
| 882 | hbuss | 393 | { |
| 394 | Mess_IntegralNick = -(Umschlag180Nick - 25000L); |
||
| 395 | Mess_IntegralNick2 = Mess_IntegralNick; |
||
| 1051 | killagreg | 396 | } |
| 397 | if(Mess_IntegralNick <-Umschlag180Nick) |
||
| 395 | hbuss | 398 | { |
| 882 | hbuss | 399 | Mess_IntegralNick = (Umschlag180Nick - 25000L); |
| 395 | hbuss | 400 | Mess_IntegralNick2 = Mess_IntegralNick; |
| 1051 | killagreg | 401 | } |
| 1111 | hbuss | 402 | |
| 1 | ingob | 403 | Integral_Gier = Mess_Integral_Gier; |
| 404 | IntegralNick = Mess_IntegralNick; |
||
| 405 | IntegralRoll = Mess_IntegralRoll; |
||
| 1051 | killagreg | 406 | IntegralNick2 = Mess_IntegralNick2; |
| 1 | ingob | 407 | IntegralRoll2 = Mess_IntegralRoll2; |
| 408 | |||
| 1166 | hbuss | 409 | #define D_LIMIT 128 |
| 410 | |||
| 1171 | hbuss | 411 | MesswertNick = HiResNick / 8; |
| 412 | MesswertRoll = HiResRoll / 8; |
||
| 1166 | hbuss | 413 | |
| 1167 | hbuss | 414 | if(AdWertNick < 15) MesswertNick = -1000; if(AdWertNick < 7) MesswertNick = -2000; |
| 415 | if(PlatinenVersion == 10) { if(AdWertNick > 1010) MesswertNick = +1000; if(AdWertNick > 1017) MesswertNick = +2000; } |
||
| 416 | else { if(AdWertNick > 2000) MesswertNick = +1000; if(AdWertNick > 2015) MesswertNick = +2000; } |
||
| 417 | if(AdWertRoll < 15) MesswertRoll = -1000; if(AdWertRoll < 7) MesswertRoll = -2000; |
||
| 418 | if(PlatinenVersion == 10) { if(AdWertRoll > 1010) MesswertRoll = +1000; if(AdWertRoll > 1017) MesswertRoll = +2000; } |
||
| 419 | else { if(AdWertRoll > 2000) MesswertRoll = +1000; if(AdWertRoll > 2015) MesswertRoll = +2000; } |
||
| 420 | |||
| 1111 | hbuss | 421 | if(Parameter_Gyro_D) |
| 422 | { |
||
| 1166 | hbuss | 423 | d2Nick = HiResNick - oldNick; |
| 424 | oldNick = (oldNick + HiResNick)/2; |
||
| 1111 | hbuss | 425 | if(d2Nick > D_LIMIT) d2Nick = D_LIMIT; |
| 426 | else if(d2Nick < -D_LIMIT) d2Nick = -D_LIMIT; |
||
| 1166 | hbuss | 427 | MesswertNick += (d2Nick * (signed int) Parameter_Gyro_D) / 16; |
| 428 | d2Roll = HiResRoll - oldRoll; |
||
| 429 | oldRoll = (oldRoll + HiResRoll)/2; |
||
| 1111 | hbuss | 430 | if(d2Roll > D_LIMIT) d2Roll = D_LIMIT; |
| 431 | else if(d2Roll < -D_LIMIT) d2Roll = -D_LIMIT; |
||
| 1166 | hbuss | 432 | MesswertRoll += (d2Roll * (signed int) Parameter_Gyro_D) / 16; |
| 433 | HiResNick += (d2Nick * (signed int) Parameter_Gyro_D); |
||
| 434 | HiResRoll += (d2Roll * (signed int) Parameter_Gyro_D); |
||
| 1111 | hbuss | 435 | } |
| 436 | |||
| 1166 | hbuss | 437 | if(RohMesswertRoll > 0) TrimRoll += ((long) abs(KopplungsteilNickRoll) * Parameter_CouplingYawCorrection) / 64L; |
| 438 | else TrimRoll -= ((long) abs(KopplungsteilNickRoll) * Parameter_CouplingYawCorrection) / 64L; |
||
| 439 | if(RohMesswertNick > 0) TrimNick += ((long) abs(KopplungsteilRollNick) * Parameter_CouplingYawCorrection) / 64L; |
||
| 440 | else TrimNick -= ((long) abs(KopplungsteilRollNick) * Parameter_CouplingYawCorrection) / 64L; |
||
| 1153 | hbuss | 441 | |
| 442 | if(EE_Parameter.GlobalConfig & CFG_DREHRATEN_BEGRENZER && !Looping_Nick && !Looping_Roll) |
||
| 443 | { |
||
| 444 | if(RohMesswertNick > 256) MesswertNick += 1 * (RohMesswertNick - 256); |
||
| 445 | else if(RohMesswertNick < -256) MesswertNick += 1 * (RohMesswertNick + 256); |
||
| 446 | if(RohMesswertRoll > 256) MesswertRoll += 1 * (RohMesswertRoll - 256); |
||
| 447 | else if(RohMesswertRoll < -256) MesswertRoll += 1 * (RohMesswertRoll + 256); |
||
| 448 | } |
||
| 449 | |||
| 1 | ingob | 450 | if(Poti1 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI1]] + 110) Poti1++; else if(Poti1 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI1]] + 110 && Poti1) Poti1--; |
| 451 | if(Poti2 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI2]] + 110) Poti2++; else if(Poti2 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI2]] + 110 && Poti2) Poti2--; |
||
| 452 | if(Poti3 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI3]] + 110) Poti3++; else if(Poti3 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI3]] + 110 && Poti3) Poti3--; |
||
| 453 | if(Poti4 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI4]] + 110) Poti4++; else if(Poti4 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI4]] + 110 && Poti4) Poti4--; |
||
| 454 | if(Poti1 < 0) Poti1 = 0; else if(Poti1 > 255) Poti1 = 255; |
||
| 455 | if(Poti2 < 0) Poti2 = 0; else if(Poti2 > 255) Poti2 = 255; |
||
| 456 | if(Poti3 < 0) Poti3 = 0; else if(Poti3 > 255) Poti3 = 255; |
||
| 457 | if(Poti4 < 0) Poti4 = 0; else if(Poti4 > 255) Poti4 = 255; |
||
| 458 | } |
||
| 459 | |||
| 460 | //############################################################################ |
||
| 461 | // Messwerte beim Ermitteln der Nullage |
||
| 462 | void CalibrierMittelwert(void) |
||
| 463 | //############################################################################ |
||
| 1051 | killagreg | 464 | { |
| 1021 | hbuss | 465 | if(PlatinenVersion == 13) SucheGyroOffset(); |
| 1 | ingob | 466 | // ADC auschalten, damit die Werte sich nicht während der Berechnung ändern |
| 467 | ANALOG_OFF; |
||
| 395 | hbuss | 468 | MesswertNick = AdWertNick; |
| 469 | MesswertRoll = AdWertRoll; |
||
| 470 | MesswertGier = AdWertGier; |
||
| 471 | Mittelwert_AccNick = ACC_AMPLIFY * (long)AdWertAccNick; |
||
| 472 | Mittelwert_AccRoll = ACC_AMPLIFY * (long)AdWertAccRoll; |
||
| 473 | Mittelwert_AccHoch = (long)AdWertAccHoch; |
||
| 474 | // ADC einschalten |
||
| 1051 | killagreg | 475 | ANALOG_ON; |
| 1 | ingob | 476 | if(Poti1 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI1]] + 110) Poti1++; else if(Poti1 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI1]] + 110 && Poti1) Poti1--; |
| 477 | if(Poti2 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI2]] + 110) Poti2++; else if(Poti2 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI2]] + 110 && Poti2) Poti2--; |
||
| 478 | if(Poti3 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI3]] + 110) Poti3++; else if(Poti3 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI3]] + 110 && Poti3) Poti3--; |
||
| 479 | if(Poti4 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI4]] + 110) Poti4++; else if(Poti4 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI4]] + 110 && Poti4) Poti4--; |
||
| 480 | if(Poti1 < 0) Poti1 = 0; else if(Poti1 > 255) Poti1 = 255; |
||
| 481 | if(Poti2 < 0) Poti2 = 0; else if(Poti2 > 255) Poti2 = 255; |
||
| 482 | if(Poti3 < 0) Poti3 = 0; else if(Poti3 > 255) Poti3 = 255; |
||
| 483 | if(Poti4 < 0) Poti4 = 0; else if(Poti4 > 255) Poti4 = 255; |
||
| 395 | hbuss | 484 | |
| 485 | Umschlag180Nick = (long) EE_Parameter.WinkelUmschlagNick * 2500L; |
||
| 720 | ingob | 486 | Umschlag180Roll = (long) EE_Parameter.WinkelUmschlagRoll * 2500L; |
| 1 | ingob | 487 | } |
| 488 | |||
| 489 | //############################################################################ |
||
| 490 | // Senden der Motorwerte per I2C-Bus |
||
| 491 | void SendMotorData(void) |
||
| 492 | //############################################################################ |
||
| 1051 | killagreg | 493 | { |
| 1209 | hbuss | 494 | unsigned char i; |
| 921 | hbuss | 495 | if(!MotorenEin) |
| 1 | ingob | 496 | { |
| 1209 | hbuss | 497 | for(i=0;i<MAX_MOTORS;i++) Motor[i] = 0; |
| 1166 | hbuss | 498 | #ifndef QUADRO |
| 1111 | hbuss | 499 | Motor1 = 0;Motor2 = 0;Motor3 = 0;Motor4 = 0;Motor5 = 0;Motor6 = 0;Motor7 = 0;Motor8 = 0; |
| 500 | if(MotorTest[0]) {Motor1 = MotorTest[0]; Motor2 = MotorTest[0];} |
||
| 501 | if(MotorTest[3]) {Motor3 = MotorTest[3]; Motor4 = MotorTest[3];} |
||
| 502 | if(MotorTest[1]) {Motor5 = MotorTest[1]; Motor6 = MotorTest[1];} |
||
| 503 | if(MotorTest[2]) {Motor7 = MotorTest[2]; Motor8 = MotorTest[2];} |
||
| 504 | #else |
||
| 505 | Motor_Hinten = 0; Motor_Vorne = 0; Motor_Rechts = 0; Motor_Links = 0; |
||
| 1 | ingob | 506 | if(MotorTest[0]) Motor_Vorne = MotorTest[0]; |
| 507 | if(MotorTest[1]) Motor_Hinten = MotorTest[1]; |
||
| 508 | if(MotorTest[2]) Motor_Links = MotorTest[2]; |
||
| 509 | if(MotorTest[3]) Motor_Rechts = MotorTest[3]; |
||
| 1111 | hbuss | 510 | #endif |
| 1209 | hbuss | 511 | if(MotorTest[0]) Motor[0] = MotorTest[0]; |
| 512 | if(MotorTest[1]) Motor[1] = MotorTest[1]; |
||
| 513 | if(MotorTest[2]) Motor[2] = MotorTest[2]; |
||
| 514 | if(MotorTest[3]) Motor[3] = MotorTest[3]; |
||
| 1111 | hbuss | 515 | |
| 921 | hbuss | 516 | MikroKopterFlags &= ~(FLAG_MOTOR_RUN | FLAG_FLY); |
| 517 | } else MikroKopterFlags |= FLAG_MOTOR_RUN; |
||
| 1 | ingob | 518 | |
| 519 | DebugOut.Analog[12] = Motor_Vorne; |
||
| 520 | DebugOut.Analog[13] = Motor_Hinten; |
||
| 521 | DebugOut.Analog[14] = Motor_Links; |
||
| 1051 | killagreg | 522 | DebugOut.Analog[15] = Motor_Rechts; |
| 1 | ingob | 523 | |
| 524 | //Start I2C Interrupt Mode |
||
| 525 | twi_state = 0; |
||
| 526 | motor = 0; |
||
| 1051 | killagreg | 527 | i2c_start(); |
| 1 | ingob | 528 | } |
| 529 | |||
| 530 | |||
| 531 | |||
| 532 | //############################################################################ |
||
| 533 | // Trägt ggf. das Poti als Parameter ein |
||
| 1051 | killagreg | 534 | void ParameterZuordnung(void) |
| 1 | ingob | 535 | //############################################################################ |
| 536 | { |
||
| 921 | hbuss | 537 | #define CHK_POTI_MM(b,a,min,max) { if(a > 250) { if(a == 251) b = Poti1; else if(a == 252) b = Poti2; else if(a == 253) b = Poti3; else if(a == 254) b = Poti4;} else b = a; if(b <= min) b = min; else if(b >= max) b = max;} |
| 538 | #define CHK_POTI(b,a,min,max) { if(a > 250) { if(a == 251) b = Poti1; else if(a == 252) b = Poti2; else if(a == 253) b = Poti3; else if(a == 254) b = Poti4;} else b = a; } |
||
| 1 | ingob | 539 | CHK_POTI(Parameter_MaxHoehe,EE_Parameter.MaxHoehe,0,255); |
| 921 | hbuss | 540 | CHK_POTI_MM(Parameter_Luftdruck_D,EE_Parameter.Luftdruck_D,0,100); |
| 541 | CHK_POTI_MM(Parameter_Hoehe_P,EE_Parameter.Hoehe_P,0,100); |
||
| 1 | ingob | 542 | CHK_POTI(Parameter_Hoehe_ACC_Wirkung,EE_Parameter.Hoehe_ACC_Wirkung,0,255); |
| 543 | CHK_POTI(Parameter_KompassWirkung,EE_Parameter.KompassWirkung,0,255); |
||
| 921 | hbuss | 544 | CHK_POTI_MM(Parameter_Gyro_P,EE_Parameter.Gyro_P,10,255); |
| 1 | ingob | 545 | CHK_POTI(Parameter_Gyro_I,EE_Parameter.Gyro_I,0,255); |
| 1120 | hbuss | 546 | CHK_POTI(Parameter_Gyro_D,EE_Parameter.Gyro_D,0,255); |
| 1051 | killagreg | 547 | CHK_POTI(Parameter_I_Faktor,EE_Parameter.I_Faktor,0,255); |
| 548 | CHK_POTI(Parameter_UserParam1,EE_Parameter.UserParam1,0,255); |
||
| 549 | CHK_POTI(Parameter_UserParam2,EE_Parameter.UserParam2,0,255); |
||
| 550 | CHK_POTI(Parameter_UserParam3,EE_Parameter.UserParam3,0,255); |
||
| 551 | CHK_POTI(Parameter_UserParam4,EE_Parameter.UserParam4,0,255); |
||
| 552 | CHK_POTI(Parameter_UserParam5,EE_Parameter.UserParam5,0,255); |
||
| 553 | CHK_POTI(Parameter_UserParam6,EE_Parameter.UserParam6,0,255); |
||
| 554 | CHK_POTI(Parameter_UserParam7,EE_Parameter.UserParam7,0,255); |
||
| 555 | CHK_POTI(Parameter_UserParam8,EE_Parameter.UserParam8,0,255); |
||
| 1 | ingob | 556 | CHK_POTI(Parameter_ServoNickControl,EE_Parameter.ServoNickControl,0,255); |
| 173 | holgerb | 557 | CHK_POTI(Parameter_LoopGasLimit,EE_Parameter.LoopGasLimit,0,255); |
| 395 | hbuss | 558 | CHK_POTI(Parameter_AchsKopplung1, EE_Parameter.AchsKopplung1,0,255); |
| 1120 | hbuss | 559 | CHK_POTI(Parameter_AchsKopplung2, EE_Parameter.AchsKopplung2,0,255); |
| 560 | CHK_POTI(Parameter_CouplingYawCorrection,EE_Parameter.CouplingYawCorrection,0,255); |
||
| 561 | // CHK_POTI(Parameter_AchsGegenKopplung1,EE_Parameter.AchsGegenKopplung1,0,255); |
||
| 499 | hbuss | 562 | CHK_POTI(Parameter_DynamicStability,EE_Parameter.DynamicStability,0,255); |
| 921 | hbuss | 563 | CHK_POTI_MM(Parameter_J16Timing,EE_Parameter.J16Timing,1,255); |
| 564 | CHK_POTI_MM(Parameter_J17Timing,EE_Parameter.J17Timing,1,255); |
||
| 565 | CHK_POTI(Parameter_ExternalControl,EE_Parameter.ExternalControl,0,255); |
||
| 1153 | hbuss | 566 | Ki = 10300 / (Parameter_I_Faktor + 1); |
| 1 | ingob | 567 | MAX_GAS = EE_Parameter.Gas_Max; |
| 568 | MIN_GAS = EE_Parameter.Gas_Min; |
||
| 569 | } |
||
| 570 | |||
| 571 | |||
| 819 | hbuss | 572 | |
| 1 | ingob | 573 | //############################################################################ |
| 574 | // |
||
| 575 | void MotorRegler(void) |
||
| 576 | //############################################################################ |
||
| 577 | { |
||
| 1209 | hbuss | 578 | int pd_ergebnis_nick,pd_ergebnis_roll,h,tmp_int; |
| 1 | ingob | 579 | int GierMischanteil,GasMischanteil; |
| 580 | static long SummeNick=0,SummeRoll=0; |
||
| 581 | static long sollGier = 0,tmp_long,tmp_long2; |
||
| 395 | hbuss | 582 | static long IntegralFehlerNick = 0; |
| 583 | static long IntegralFehlerRoll = 0; |
||
| 1 | ingob | 584 | static unsigned int RcLostTimer; |
| 585 | static unsigned char delay_neutral = 0; |
||
| 586 | static unsigned char delay_einschalten = 0,delay_ausschalten = 0; |
||
| 587 | static int hoehenregler = 0; |
||
| 1209 | hbuss | 588 | // static int motorwert1,motorwert2,motorwert3,motorwert4,motorwert5,motorwert6,motorwert7,motorwert8; |
| 1 | ingob | 589 | static char TimerWerteausgabe = 0; |
| 590 | static char NeueKompassRichtungMerken = 0; |
||
| 395 | hbuss | 591 | static long ausgleichNick, ausgleichRoll; |
| 1153 | hbuss | 592 | int IntegralNickMalFaktor,IntegralRollMalFaktor; |
| 1209 | hbuss | 593 | unsigned char i; |
| 1051 | killagreg | 594 | Mittelwert(); |
| 595 | |||
| 1 | ingob | 596 | GRN_ON; |
| 1051 | killagreg | 597 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 598 | // Gaswert ermitteln |
| 1051 | killagreg | 599 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 600 | GasMischanteil = StickGas; |
||
| 831 | hbuss | 601 | if(GasMischanteil < MIN_GAS + 10) GasMischanteil = MIN_GAS + 10; |
| 1051 | killagreg | 602 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 693 | hbuss | 603 | // Empfang schlecht |
| 1051 | killagreg | 604 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 605 | if(SenderOkay < 100) |
| 606 | { |
||
| 1051 | killagreg | 607 | if(!PcZugriff) |
| 173 | holgerb | 608 | { |
| 1051 | killagreg | 609 | if(BeepMuster == 0xffff) |
| 610 | { |
||
| 173 | holgerb | 611 | beeptime = 15000; |
| 612 | BeepMuster = 0x0c00; |
||
| 1051 | killagreg | 613 | } |
| 173 | holgerb | 614 | } |
| 1051 | killagreg | 615 | if(RcLostTimer) RcLostTimer--; |
| 616 | else |
||
| 1 | ingob | 617 | { |
| 618 | MotorenEin = 0; |
||
| 619 | Notlandung = 0; |
||
| 1051 | killagreg | 620 | } |
| 1 | ingob | 621 | ROT_ON; |
| 693 | hbuss | 622 | if(modell_fliegt > 1000) // wahrscheinlich in der Luft --> langsam absenken |
| 1 | ingob | 623 | { |
| 624 | GasMischanteil = EE_Parameter.NotGas; |
||
| 625 | Notlandung = 1; |
||
| 744 | hbuss | 626 | PPM_diff[EE_Parameter.Kanalbelegung[K_NICK]] = 0; |
| 1051 | killagreg | 627 | PPM_diff[EE_Parameter.Kanalbelegung[K_ROLL]] = 0; |
| 1 | ingob | 628 | PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] = 0; |
| 629 | PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] = 0; |
||
| 630 | PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] = 0; |
||
| 173 | holgerb | 631 | } |
| 1 | ingob | 632 | else MotorenEin = 0; |
| 633 | } |
||
| 1051 | killagreg | 634 | else |
| 635 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1 | ingob | 636 | // Emfang gut |
| 1051 | killagreg | 637 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 638 | if(SenderOkay > 140) |
| 639 | { |
||
| 640 | Notlandung = 0; |
||
| 641 | RcLostTimer = EE_Parameter.NotGasZeit * 50; |
||
| 921 | hbuss | 642 | if(GasMischanteil > 40 && MotorenEin) |
| 1 | ingob | 643 | { |
| 644 | if(modell_fliegt < 0xffff) modell_fliegt++; |
||
| 645 | } |
||
| 871 | hbuss | 646 | if((modell_fliegt < 256)) |
| 1 | ingob | 647 | { |
| 648 | SummeNick = 0; |
||
| 649 | SummeRoll = 0; |
||
| 1051 | killagreg | 650 | if(modell_fliegt == 250) |
| 918 | hbuss | 651 | { |
| 1051 | killagreg | 652 | NeueKompassRichtungMerken = 1; |
| 918 | hbuss | 653 | sollGier = 0; |
| 1051 | killagreg | 654 | Mess_Integral_Gier = 0; |
| 927 | hbuss | 655 | // Mess_Integral_Gier2 = 0; |
| 1051 | killagreg | 656 | } |
| 921 | hbuss | 657 | } else MikroKopterFlags |= FLAG_FLY; |
| 1051 | killagreg | 658 | |
| 595 | hbuss | 659 | if((PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] > 80) && MotorenEin == 0) |
| 1 | ingob | 660 | { |
| 1051 | killagreg | 661 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 662 | // auf Nullwerte kalibrieren |
| 1051 | killagreg | 663 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 664 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] > 75) // Neutralwerte |
| 665 | { |
||
| 666 | if(++delay_neutral > 200) // nicht sofort |
||
| 667 | { |
||
| 668 | GRN_OFF; |
||
| 669 | MotorenEin = 0; |
||
| 670 | delay_neutral = 0; |
||
| 671 | modell_fliegt = 0; |
||
| 672 | if(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70 || abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) > 70) |
||
| 673 | { |
||
| 304 | ingob | 674 | unsigned char setting=1; |
| 1 | ingob | 675 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < 70) setting = 1; |
| 676 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 2; |
||
| 677 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 3; |
||
| 678 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] <-70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 4; |
||
| 679 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] <-70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < 70) setting = 5; |
||
| 1063 | killagreg | 680 | SetActiveParamSetNumber(setting); // aktiven Datensatz merken |
| 1 | ingob | 681 | } |
| 820 | hbuss | 682 | // else |
| 1051 | killagreg | 683 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) < 30 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < -70) |
| 684 | { |
||
| 819 | hbuss | 685 | WinkelOut.CalcState = 1; |
| 686 | beeptime = 1000; |
||
| 687 | } |
||
| 688 | else |
||
| 1 | ingob | 689 | { |
| 819 | hbuss | 690 | ReadParameterSet(GetActiveParamSetNumber(), (unsigned char *) &EE_Parameter.Kanalbelegung[0], STRUCT_PARAM_LAENGE); |
| 691 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG)) // Höhenregelung aktiviert? |
||
| 692 | { |
||
| 1 | ingob | 693 | if((MessLuftdruck > 950) || (MessLuftdruck < 750)) SucheLuftruckOffset(); |
| 1051 | killagreg | 694 | } |
| 819 | hbuss | 695 | SetNeutral(); |
| 696 | Piep(GetActiveParamSetNumber()); |
||
| 697 | } |
||
| 1051 | killagreg | 698 | } |
| 1 | ingob | 699 | } |
| 1051 | killagreg | 700 | else |
| 513 | hbuss | 701 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] < -75) // ACC Neutralwerte speichern |
| 702 | { |
||
| 703 | if(++delay_neutral > 200) // nicht sofort |
||
| 704 | { |
||
| 705 | GRN_OFF; |
||
| 706 | eeprom_write_byte(&EEPromArray[EEPROM_ADR_ACC_NICK],0xff); // Werte löschen |
||
| 707 | MotorenEin = 0; |
||
| 708 | delay_neutral = 0; |
||
| 709 | modell_fliegt = 0; |
||
| 710 | SetNeutral(); |
||
| 711 | eeprom_write_byte(&EEPromArray[EEPROM_ADR_ACC_NICK],NeutralAccX / 256); // ACC-NeutralWerte speichern |
||
| 712 | eeprom_write_byte(&EEPromArray[EEPROM_ADR_ACC_NICK+1],NeutralAccX % 256); // ACC-NeutralWerte speichern |
||
| 713 | eeprom_write_byte(&EEPromArray[EEPROM_ADR_ACC_ROLL],NeutralAccY / 256); |
||
| 714 | eeprom_write_byte(&EEPromArray[EEPROM_ADR_ACC_ROLL+1],NeutralAccY % 256); |
||
| 715 | eeprom_write_byte(&EEPromArray[EEPROM_ADR_ACC_Z],(int)NeutralAccZ / 256); |
||
| 716 | eeprom_write_byte(&EEPromArray[EEPROM_ADR_ACC_Z+1],(int)NeutralAccZ % 256); |
||
| 717 | Piep(GetActiveParamSetNumber()); |
||
| 1051 | killagreg | 718 | } |
| 513 | hbuss | 719 | } |
| 1 | ingob | 720 | else delay_neutral = 0; |
| 721 | } |
||
| 1051 | killagreg | 722 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 723 | // Gas ist unten |
| 1051 | killagreg | 724 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 595 | hbuss | 725 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] < 35-120) |
| 1 | ingob | 726 | { |
| 727 | // Starten |
||
| 728 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] < -75) |
||
| 729 | { |
||
| 1051 | killagreg | 730 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 731 | // Einschalten |
| 1051 | killagreg | 732 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 733 | if(++delay_einschalten > 200) |
| 734 | { |
||
| 735 | delay_einschalten = 200; |
||
| 736 | modell_fliegt = 1; |
||
| 737 | MotorenEin = 1; |
||
| 738 | sollGier = 0; |
||
| 1051 | killagreg | 739 | Mess_Integral_Gier = 0; |
| 1 | ingob | 740 | Mess_Integral_Gier2 = 0; |
| 1173 | hbuss | 741 | Mess_IntegralNick = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccNick; |
| 742 | Mess_IntegralRoll = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccRoll; |
||
| 1 | ingob | 743 | Mess_IntegralNick2 = IntegralNick; |
| 744 | Mess_IntegralRoll2 = IntegralRoll; |
||
| 745 | SummeNick = 0; |
||
| 746 | SummeRoll = 0; |
||
| 921 | hbuss | 747 | MikroKopterFlags |= FLAG_START; |
| 1051 | killagreg | 748 | } |
| 749 | } |
||
| 1 | ingob | 750 | else delay_einschalten = 0; |
| 751 | //Auf Neutralwerte setzen |
||
| 1051 | killagreg | 752 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 753 | // Auschalten |
| 1051 | killagreg | 754 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 755 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] > 75) |
| 756 | { |
||
| 757 | if(++delay_ausschalten > 200) // nicht sofort |
||
| 758 | { |
||
| 759 | MotorenEin = 0; |
||
| 760 | delay_ausschalten = 200; |
||
| 761 | modell_fliegt = 0; |
||
| 1051 | killagreg | 762 | } |
| 1 | ingob | 763 | } |
| 764 | else delay_ausschalten = 0; |
||
| 765 | } |
||
| 766 | } |
||
| 767 | |||
| 1051 | killagreg | 768 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 769 | // neue Werte von der Funke |
| 1051 | killagreg | 770 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1153 | hbuss | 771 | |
| 1051 | killagreg | 772 | if(!NewPpmData-- || Notlandung) |
| 1 | ingob | 773 | { |
| 492 | hbuss | 774 | int tmp_int; |
| 604 | hbuss | 775 | static int stick_nick,stick_roll; |
| 1 | ingob | 776 | ParameterZuordnung(); |
| 1051 | killagreg | 777 | stick_nick = (stick_nick * 3 + PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] * EE_Parameter.Stick_P) / 4; |
| 723 | hbuss | 778 | stick_nick += PPM_diff[EE_Parameter.Kanalbelegung[K_NICK]] * EE_Parameter.Stick_D; |
| 805 | hbuss | 779 | StickNick = stick_nick - (GPS_Nick + GPS_Nick2); |
| 604 | hbuss | 780 | |
| 723 | hbuss | 781 | stick_roll = (stick_roll * 3 + PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] * EE_Parameter.Stick_P) / 4; |
| 782 | stick_roll += PPM_diff[EE_Parameter.Kanalbelegung[K_ROLL]] * EE_Parameter.Stick_D; |
||
| 805 | hbuss | 783 | StickRoll = stick_roll - (GPS_Roll + GPS_Roll2); |
| 723 | hbuss | 784 | |
| 1 | ingob | 785 | StickGier = -PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]; |
| 1120 | hbuss | 786 | if(StickGier > 2) StickGier -= 2; else |
| 787 | if(StickGier < -2) StickGier += 2; else StickGier = 0; |
||
| 788 | |||
| 595 | hbuss | 789 | StickGas = PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] + 120; |
| 790 | |||
| 1051 | killagreg | 791 | /* if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]]) > MaxStickNick) |
| 614 | hbuss | 792 | MaxStickNick = abs(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]]); else MaxStickNick--; |
| 1051 | killagreg | 793 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) > MaxStickRoll) |
| 614 | hbuss | 794 | MaxStickRoll = abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]); else MaxStickRoll--; |
| 723 | hbuss | 795 | */ |
| 1153 | hbuss | 796 | // GyroFaktor = ((float)Parameter_Gyro_P + 10.0) / (256.0/STICK_GAIN); |
| 797 | GyroFaktor = (Parameter_Gyro_P + 10.0); |
||
| 798 | // IntegralFaktor = ((float) Parameter_Gyro_I) / (44000 / STICK_GAIN); |
||
| 799 | IntegralFaktor = Parameter_Gyro_I; |
||
| 1 | ingob | 800 | |
| 595 | hbuss | 801 | //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 802 | //+ Analoge Steuerung per Seriell |
||
| 803 | //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 921 | hbuss | 804 | if(ExternControl.Config & 0x01 && Parameter_ExternalControl > 128) |
| 595 | hbuss | 805 | { |
| 806 | StickNick += (int) ExternControl.Nick * (int) EE_Parameter.Stick_P; |
||
| 807 | StickRoll += (int) ExternControl.Roll * (int) EE_Parameter.Stick_P; |
||
| 808 | StickGier += ExternControl.Gier; |
||
| 809 | ExternHoehenValue = (int) ExternControl.Hight * (int)EE_Parameter.Hoehe_Verstaerkung; |
||
| 810 | if(ExternControl.Gas < StickGas) StickGas = ExternControl.Gas; |
||
| 811 | } |
||
| 855 | hbuss | 812 | if(StickGas < 0) StickGas = 0; |
| 492 | hbuss | 813 | |
| 1 | ingob | 814 | if(EE_Parameter.GlobalConfig & CFG_HEADING_HOLD) IntegralFaktor = 0; |
| 815 | if(GyroFaktor < 0) GyroFaktor = 0; |
||
| 816 | if(IntegralFaktor < 0) IntegralFaktor = 0; |
||
| 723 | hbuss | 817 | |
| 1051 | killagreg | 818 | if(abs(StickNick/STICK_GAIN) > MaxStickNick) |
| 928 | hbuss | 819 | { |
| 1051 | killagreg | 820 | MaxStickNick = abs(StickNick)/STICK_GAIN; |
| 928 | hbuss | 821 | if(MaxStickNick > 100) MaxStickNick = 100; |
| 1051 | killagreg | 822 | } |
| 928 | hbuss | 823 | else MaxStickNick--; |
| 1051 | killagreg | 824 | if(abs(StickRoll/STICK_GAIN) > MaxStickRoll) |
| 928 | hbuss | 825 | { |
| 1051 | killagreg | 826 | MaxStickRoll = abs(StickRoll)/STICK_GAIN; |
| 928 | hbuss | 827 | if(MaxStickRoll > 100) MaxStickRoll = 100; |
| 1051 | killagreg | 828 | } |
| 928 | hbuss | 829 | else MaxStickRoll--; |
| 723 | hbuss | 830 | if(Notlandung) {MaxStickNick = 0; MaxStickRoll = 0;} |
| 831 | |||
| 1051 | killagreg | 832 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 173 | holgerb | 833 | // Looping? |
| 1051 | killagreg | 834 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 993 | hbuss | 835 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_LINKS) Looping_Links = 1; |
| 1051 | killagreg | 836 | else |
| 837 | { |
||
| 395 | hbuss | 838 | { |
| 1051 | killagreg | 839 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < (EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese))) Looping_Links = 0; |
| 840 | } |
||
| 841 | } |
||
| 993 | hbuss | 842 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < -EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_RECHTS) Looping_Rechts = 1; |
| 1051 | killagreg | 843 | else |
| 395 | hbuss | 844 | { |
| 845 | if(Looping_Rechts) // Hysterese |
||
| 846 | { |
||
| 847 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > -(EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese)) Looping_Rechts = 0; |
||
| 848 | } |
||
| 1051 | killagreg | 849 | } |
| 173 | holgerb | 850 | |
| 993 | hbuss | 851 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_OBEN) Looping_Oben = 1; |
| 1051 | killagreg | 852 | else |
| 853 | { |
||
| 395 | hbuss | 854 | if(Looping_Oben) // Hysterese |
| 855 | { |
||
| 1051 | killagreg | 856 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < (EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese))) Looping_Oben = 0; |
| 857 | } |
||
| 858 | } |
||
| 993 | hbuss | 859 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < -EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_UNTEN) Looping_Unten = 1; |
| 1051 | killagreg | 860 | else |
| 395 | hbuss | 861 | { |
| 862 | if(Looping_Unten) // Hysterese |
||
| 863 | { |
||
| 864 | if(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > -(EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese)) Looping_Unten = 0; |
||
| 865 | } |
||
| 1051 | killagreg | 866 | } |
| 395 | hbuss | 867 | |
| 868 | if(Looping_Links || Looping_Rechts) Looping_Roll = 1; else Looping_Roll = 0; |
||
| 1153 | hbuss | 869 | if(Looping_Oben || Looping_Unten) { Looping_Nick = 1; Looping_Roll = 0; Looping_Links = 0; Looping_Rechts = 0;} else Looping_Nick = 0; |
| 395 | hbuss | 870 | } // Ende neue Funken-Werte |
| 871 | |||
| 872 | if(Looping_Roll || Looping_Nick) |
||
| 873 | { |
||
| 173 | holgerb | 874 | if(GasMischanteil > EE_Parameter.LoopGasLimit) GasMischanteil = EE_Parameter.LoopGasLimit; |
| 1153 | hbuss | 875 | TrichterFlug = 1; |
| 173 | holgerb | 876 | } |
| 877 | |||
| 1051 | killagreg | 878 | |
| 879 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 880 | // Bei Empfangsausfall im Flug |
||
| 881 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1 | ingob | 882 | if(Notlandung) |
| 883 | { |
||
| 884 | StickGier = 0; |
||
| 885 | StickNick = 0; |
||
| 886 | StickRoll = 0; |
||
| 1153 | hbuss | 887 | GyroFaktor = 90;//(float) 100 / (256.0 / STICK_GAIN); |
| 888 | IntegralFaktor = 120;//(float) 120 / (44000 / STICK_GAIN); |
||
| 173 | holgerb | 889 | Looping_Roll = 0; |
| 890 | Looping_Nick = 0; |
||
| 1051 | killagreg | 891 | } |
| 395 | hbuss | 892 | |
| 893 | |||
| 1051 | killagreg | 894 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 895 | // Integrale auf ACC-Signal abgleichen |
| 1051 | killagreg | 896 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 395 | hbuss | 897 | #define ABGLEICH_ANZAHL 256L |
| 898 | |||
| 899 | MittelIntegralNick += IntegralNick; // Für die Mittelwertbildung aufsummieren |
||
| 900 | MittelIntegralRoll += IntegralRoll; |
||
| 901 | MittelIntegralNick2 += IntegralNick2; |
||
| 902 | MittelIntegralRoll2 += IntegralRoll2; |
||
| 903 | |||
| 904 | if(Looping_Nick || Looping_Roll) |
||
| 905 | { |
||
| 906 | IntegralAccNick = 0; |
||
| 907 | IntegralAccRoll = 0; |
||
| 908 | MittelIntegralNick = 0; |
||
| 909 | MittelIntegralRoll = 0; |
||
| 910 | MittelIntegralNick2 = 0; |
||
| 911 | MittelIntegralRoll2 = 0; |
||
| 912 | Mess_IntegralNick2 = Mess_IntegralNick; |
||
| 913 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
||
| 914 | ZaehlMessungen = 0; |
||
| 498 | hbuss | 915 | LageKorrekturNick = 0; |
| 916 | LageKorrekturRoll = 0; |
||
| 395 | hbuss | 917 | } |
| 918 | |||
| 1051 | killagreg | 919 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1172 | hbuss | 920 | if(!Looping_Nick && !Looping_Roll && Aktuell_az > 512) |
| 469 | hbuss | 921 | { |
| 922 | long tmp_long, tmp_long2; |
||
| 1171 | hbuss | 923 | if(FromNaviCtrl_Value.Kalman_K != -1 /*&& !TrichterFlug*/) |
| 992 | hbuss | 924 | { |
| 925 | tmp_long = (long)(IntegralNick / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccNick); |
||
| 1051 | killagreg | 926 | tmp_long2 = (long)(IntegralRoll / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccRoll); |
| 927 | tmp_long = (tmp_long * FromNaviCtrl_Value.Kalman_K) / (32 * 16); |
||
| 928 | tmp_long2 = (tmp_long2 * FromNaviCtrl_Value.Kalman_K) / (32 * 16); |
||
| 992 | hbuss | 929 | if((MaxStickNick > 64) || (MaxStickRoll > 64)) |
| 930 | { |
||
| 931 | tmp_long /= 2; |
||
| 932 | tmp_long2 /= 2; |
||
| 933 | } |
||
| 934 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25) |
||
| 935 | { |
||
| 936 | tmp_long /= 3; |
||
| 937 | tmp_long2 /= 3; |
||
| 938 | } |
||
| 939 | if(tmp_long > (long) FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long = (long) FromNaviCtrl_Value.Kalman_MaxFusion; |
||
| 940 | if(tmp_long < (long)-FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long = (long)-FromNaviCtrl_Value.Kalman_MaxFusion; |
||
| 941 | if(tmp_long2 > (long) FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long2 = (long) FromNaviCtrl_Value.Kalman_MaxFusion; |
||
| 942 | if(tmp_long2 < (long)-FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long2 = (long)-FromNaviCtrl_Value.Kalman_MaxFusion; |
||
| 943 | } |
||
| 1051 | killagreg | 944 | else |
| 992 | hbuss | 945 | { |
| 946 | tmp_long = (long)(IntegralNick / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccNick); |
||
| 1051 | killagreg | 947 | tmp_long2 = (long)(IntegralRoll / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccRoll); |
| 992 | hbuss | 948 | tmp_long /= 16; |
| 949 | tmp_long2 /= 16; |
||
| 950 | if((MaxStickNick > 64) || (MaxStickRoll > 64)) |
||
| 951 | { |
||
| 952 | tmp_long /= 3; |
||
| 953 | tmp_long2 /= 3; |
||
| 1171 | hbuss | 954 | } |
| 1120 | hbuss | 955 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25) |
| 992 | hbuss | 956 | { |
| 957 | tmp_long /= 3; |
||
| 958 | tmp_long2 /= 3; |
||
| 959 | } |
||
| 1155 | hbuss | 960 | |
| 961 | #define AUSGLEICH 32 |
||
| 992 | hbuss | 962 | if(tmp_long > AUSGLEICH) tmp_long = AUSGLEICH; |
| 963 | if(tmp_long < -AUSGLEICH) tmp_long =-AUSGLEICH; |
||
| 964 | if(tmp_long2 > AUSGLEICH) tmp_long2 = AUSGLEICH; |
||
| 965 | if(tmp_long2 <-AUSGLEICH) tmp_long2 =-AUSGLEICH; |
||
| 966 | } |
||
| 1166 | hbuss | 967 | |
| 968 | //if(Poti2 > 20) { tmp_long = 0; tmp_long2 = 0;} |
||
| 1111 | hbuss | 969 | Mess_IntegralNick -= tmp_long; |
| 970 | Mess_IntegralRoll -= tmp_long2; |
||
| 469 | hbuss | 971 | } |
| 1051 | killagreg | 972 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 395 | hbuss | 973 | if(ZaehlMessungen >= ABGLEICH_ANZAHL) |
| 974 | { |
||
| 975 | static int cnt = 0; |
||
| 976 | static char last_n_p,last_n_n,last_r_p,last_r_n; |
||
| 977 | static long MittelIntegralNick_Alt,MittelIntegralRoll_Alt; |
||
| 1173 | hbuss | 978 | if(!Looping_Nick && !Looping_Roll && !TrichterFlug && EE_Parameter.Driftkomp) |
| 173 | holgerb | 979 | { |
| 395 | hbuss | 980 | MittelIntegralNick /= ABGLEICH_ANZAHL; |
| 981 | MittelIntegralRoll /= ABGLEICH_ANZAHL; |
||
| 982 | IntegralAccNick = (EE_Parameter.GyroAccFaktor * IntegralAccNick) / ABGLEICH_ANZAHL; |
||
| 983 | IntegralAccRoll = (EE_Parameter.GyroAccFaktor * IntegralAccRoll) / ABGLEICH_ANZAHL; |
||
| 984 | IntegralAccZ = IntegralAccZ / ABGLEICH_ANZAHL; |
||
| 492 | hbuss | 985 | #define MAX_I 0//(Poti2/10) |
| 395 | hbuss | 986 | // Nick ++++++++++++++++++++++++++++++++++++++++++++++++ |
| 987 | IntegralFehlerNick = (long)(MittelIntegralNick - (long)IntegralAccNick); |
||
| 988 | ausgleichNick = IntegralFehlerNick / EE_Parameter.GyroAccAbgleich; |
||
| 1051 | killagreg | 989 | // Roll ++++++++++++++++++++++++++++++++++++++++++++++++ |
| 990 | IntegralFehlerRoll = (long)(MittelIntegralRoll - (long)IntegralAccRoll); |
||
| 395 | hbuss | 991 | ausgleichRoll = IntegralFehlerRoll / EE_Parameter.GyroAccAbgleich; |
| 614 | hbuss | 992 | |
| 993 | LageKorrekturNick = ausgleichNick / ABGLEICH_ANZAHL; |
||
| 498 | hbuss | 994 | LageKorrekturRoll = ausgleichRoll / ABGLEICH_ANZAHL; |
| 395 | hbuss | 995 | |
| 992 | hbuss | 996 | if(((MaxStickNick > 64) || (MaxStickRoll > 64) || (abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25)) && (FromNaviCtrl_Value.Kalman_K == -1)) |
| 614 | hbuss | 997 | { |
| 998 | LageKorrekturNick /= 2; |
||
| 720 | ingob | 999 | LageKorrekturRoll /= 2; |
| 614 | hbuss | 1000 | } |
| 498 | hbuss | 1001 | |
| 1051 | killagreg | 1002 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 395 | hbuss | 1003 | // Gyro-Drift ermitteln |
| 1051 | killagreg | 1004 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 395 | hbuss | 1005 | MittelIntegralNick2 /= ABGLEICH_ANZAHL; |
| 1006 | MittelIntegralRoll2 /= ABGLEICH_ANZAHL; |
||
| 1051 | killagreg | 1007 | tmp_long = IntegralNick2 - IntegralNick; |
| 1008 | tmp_long2 = IntegralRoll2 - IntegralRoll; |
||
| 395 | hbuss | 1009 | //DebugOut.Analog[25] = MittelIntegralRoll2 / 26; |
| 1010 | |||
| 1011 | IntegralFehlerNick = tmp_long; |
||
| 1012 | IntegralFehlerRoll = tmp_long2; |
||
| 1013 | Mess_IntegralNick2 -= IntegralFehlerNick; |
||
| 1014 | Mess_IntegralRoll2 -= IntegralFehlerRoll; |
||
| 1015 | |||
| 1016 | // IntegralFehlerNick = (IntegralFehlerNick * 1 + tmp_long) / 2; |
||
| 1017 | // IntegralFehlerRoll = (IntegralFehlerRoll * 1 + tmp_long2) / 2; |
||
| 1111 | hbuss | 1018 | if(EE_Parameter.Driftkomp) |
| 1019 | { |
||
| 927 | hbuss | 1020 | if(GierGyroFehler > ABGLEICH_ANZAHL/2) { AdNeutralGier++; AdNeutralGierBias++; } |
| 1021 | if(GierGyroFehler <-ABGLEICH_ANZAHL/2) { AdNeutralGier--; AdNeutralGierBias--; } |
||
| 1111 | hbuss | 1022 | } |
| 1153 | hbuss | 1023 | //DebugOut.Analog[22] = MittelIntegralRoll / 26; |
| 921 | hbuss | 1024 | //DebugOut.Analog[24] = GierGyroFehler; |
| 693 | hbuss | 1025 | GierGyroFehler = 0; |
| 720 | ingob | 1026 | |
| 1027 | |||
| 1028 | /*DebugOut.Analog[17] = IntegralAccNick / 26; |
||
| 395 | hbuss | 1029 | DebugOut.Analog[18] = IntegralAccRoll / 26; |
| 1030 | DebugOut.Analog[19] = IntegralFehlerNick;// / 26; |
||
| 1031 | DebugOut.Analog[20] = IntegralFehlerRoll;// / 26; |
||
| 720 | ingob | 1032 | */ |
| 1033 | //DebugOut.Analog[21] = MittelIntegralNick / 26; |
||
| 1034 | //MittelIntegralRoll = MittelIntegralRoll; |
||
| 469 | hbuss | 1035 | //DebugOut.Analog[28] = ausgleichNick; |
| 720 | ingob | 1036 | /* |
| 395 | hbuss | 1037 | DebugOut.Analog[29] = ausgleichRoll; |
| 498 | hbuss | 1038 | DebugOut.Analog[30] = LageKorrekturRoll * 10; |
| 720 | ingob | 1039 | */ |
| 395 | hbuss | 1040 | |
| 492 | hbuss | 1041 | #define FEHLER_LIMIT (ABGLEICH_ANZAHL * 4) |
| 1042 | #define FEHLER_LIMIT2 (ABGLEICH_ANZAHL * 16) |
||
| 1043 | #define BEWEGUNGS_LIMIT 20000 |
||
| 395 | hbuss | 1044 | // Nick +++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1045 | cnt = 1;// + labs(IntegralFehlerNick) / 4096; |
||
| 1173 | hbuss | 1046 | if(labs(MittelIntegralNick_Alt - MittelIntegralNick) < BEWEGUNGS_LIMIT || (FromNaviCtrl_Value.Kalman_MaxDrift > 3*8)) |
| 492 | hbuss | 1047 | { |
| 1051 | killagreg | 1048 | if(IntegralFehlerNick > FEHLER_LIMIT2) |
| 395 | hbuss | 1049 | { |
| 1051 | killagreg | 1050 | if(last_n_p) |
| 395 | hbuss | 1051 | { |
| 1173 | hbuss | 1052 | cnt += labs(IntegralFehlerNick) / (FEHLER_LIMIT2 / 8); |
| 492 | hbuss | 1053 | ausgleichNick = IntegralFehlerNick / 8; |
| 401 | hbuss | 1054 | if(ausgleichNick > 5000) ausgleichNick = 5000; |
| 498 | hbuss | 1055 | LageKorrekturNick += ausgleichNick / ABGLEICH_ANZAHL; |
| 1051 | killagreg | 1056 | } |
| 395 | hbuss | 1057 | else last_n_p = 1; |
| 1058 | } else last_n_p = 0; |
||
| 1051 | killagreg | 1059 | if(IntegralFehlerNick < -FEHLER_LIMIT2) |
| 395 | hbuss | 1060 | { |
| 1061 | if(last_n_n) |
||
| 1051 | killagreg | 1062 | { |
| 1173 | hbuss | 1063 | cnt += labs(IntegralFehlerNick) / (FEHLER_LIMIT2 / 8); |
| 492 | hbuss | 1064 | ausgleichNick = IntegralFehlerNick / 8; |
| 401 | hbuss | 1065 | if(ausgleichNick < -5000) ausgleichNick = -5000; |
| 498 | hbuss | 1066 | LageKorrekturNick += ausgleichNick / ABGLEICH_ANZAHL; |
| 1051 | killagreg | 1067 | } |
| 395 | hbuss | 1068 | else last_n_n = 1; |
| 1069 | } else last_n_n = 0; |
||
| 1051 | killagreg | 1070 | } |
| 1071 | else |
||
| 847 | hbuss | 1072 | { |
| 1073 | cnt = 0; |
||
| 921 | hbuss | 1074 | KompassSignalSchlecht = 1000; |
| 1051 | killagreg | 1075 | } |
| 499 | hbuss | 1076 | if(cnt > EE_Parameter.Driftkomp) cnt = EE_Parameter.Driftkomp; |
| 1173 | hbuss | 1077 | if(FromNaviCtrl_Value.Kalman_MaxDrift) if(cnt > FromNaviCtrl_Value.Kalman_MaxDrift) cnt = FromNaviCtrl_Value.Kalman_MaxDrift; |
| 395 | hbuss | 1078 | if(IntegralFehlerNick > FEHLER_LIMIT) AdNeutralNick += cnt; |
| 1079 | if(IntegralFehlerNick < -FEHLER_LIMIT) AdNeutralNick -= cnt; |
||
| 401 | hbuss | 1080 | |
| 395 | hbuss | 1081 | // Roll +++++++++++++++++++++++++++++++++++++++++++++++++ |
| 492 | hbuss | 1082 | cnt = 1;// + labs(IntegralFehlerNick) / 4096; |
| 1083 | |||
| 498 | hbuss | 1084 | ausgleichRoll = 0; |
| 1173 | hbuss | 1085 | if(labs(MittelIntegralRoll_Alt - MittelIntegralRoll) < BEWEGUNGS_LIMIT || (FromNaviCtrl_Value.Kalman_MaxDrift > 3*8)) |
| 492 | hbuss | 1086 | { |
| 1051 | killagreg | 1087 | if(IntegralFehlerRoll > FEHLER_LIMIT2) |
| 395 | hbuss | 1088 | { |
| 1051 | killagreg | 1089 | if(last_r_p) |
| 395 | hbuss | 1090 | { |
| 1173 | hbuss | 1091 | cnt += labs(IntegralFehlerRoll) / (FEHLER_LIMIT2 / 8); |
| 492 | hbuss | 1092 | ausgleichRoll = IntegralFehlerRoll / 8; |
| 401 | hbuss | 1093 | if(ausgleichRoll > 5000) ausgleichRoll = 5000; |
| 498 | hbuss | 1094 | LageKorrekturRoll += ausgleichRoll / ABGLEICH_ANZAHL; |
| 1051 | killagreg | 1095 | } |
| 395 | hbuss | 1096 | else last_r_p = 1; |
| 1097 | } else last_r_p = 0; |
||
| 1051 | killagreg | 1098 | if(IntegralFehlerRoll < -FEHLER_LIMIT2) |
| 395 | hbuss | 1099 | { |
| 1051 | killagreg | 1100 | if(last_r_n) |
| 395 | hbuss | 1101 | { |
| 1173 | hbuss | 1102 | cnt += labs(IntegralFehlerRoll) / (FEHLER_LIMIT2 / 8); |
| 492 | hbuss | 1103 | ausgleichRoll = IntegralFehlerRoll / 8; |
| 401 | hbuss | 1104 | if(ausgleichRoll < -5000) ausgleichRoll = -5000; |
| 498 | hbuss | 1105 | LageKorrekturRoll += ausgleichRoll / ABGLEICH_ANZAHL; |
| 395 | hbuss | 1106 | } |
| 1107 | else last_r_n = 1; |
||
| 1108 | } else last_r_n = 0; |
||
| 1051 | killagreg | 1109 | } else |
| 492 | hbuss | 1110 | { |
| 1111 | cnt = 0; |
||
| 921 | hbuss | 1112 | KompassSignalSchlecht = 1000; |
| 1051 | killagreg | 1113 | } |
| 499 | hbuss | 1114 | if(cnt > EE_Parameter.Driftkomp) cnt = EE_Parameter.Driftkomp; |
| 1173 | hbuss | 1115 | if(FromNaviCtrl_Value.Kalman_MaxDrift) if(cnt > FromNaviCtrl_Value.Kalman_MaxDrift) cnt = FromNaviCtrl_Value.Kalman_MaxDrift; |
| 395 | hbuss | 1116 | if(IntegralFehlerRoll > FEHLER_LIMIT) AdNeutralRoll += cnt; |
| 1117 | if(IntegralFehlerRoll < -FEHLER_LIMIT) AdNeutralRoll -= cnt; |
||
| 173 | holgerb | 1118 | } |
| 1051 | killagreg | 1119 | else |
| 498 | hbuss | 1120 | { |
| 1121 | LageKorrekturRoll = 0; |
||
| 1122 | LageKorrekturNick = 0; |
||
| 880 | hbuss | 1123 | TrichterFlug = 0; |
| 498 | hbuss | 1124 | } |
| 1051 | killagreg | 1125 | |
| 498 | hbuss | 1126 | if(!IntegralFaktor) { LageKorrekturRoll = 0; LageKorrekturNick = 0;} // z.B. bei HH |
| 1051 | killagreg | 1127 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1128 | MittelIntegralNick_Alt = MittelIntegralNick; |
||
| 1129 | MittelIntegralRoll_Alt = MittelIntegralRoll; |
||
| 1130 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 395 | hbuss | 1131 | IntegralAccNick = 0; |
| 1132 | IntegralAccRoll = 0; |
||
| 1133 | IntegralAccZ = 0; |
||
| 1134 | MittelIntegralNick = 0; |
||
| 1135 | MittelIntegralRoll = 0; |
||
| 1136 | MittelIntegralNick2 = 0; |
||
| 1137 | MittelIntegralRoll2 = 0; |
||
| 1138 | ZaehlMessungen = 0; |
||
| 1173 | hbuss | 1139 | } // ZaehlMessungen >= ABGLEICH_ANZAHL |
| 395 | hbuss | 1140 | |
| 1173 | hbuss | 1141 | |
| 1051 | killagreg | 1142 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 1143 | // Gieren |
| 1051 | killagreg | 1144 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 693 | hbuss | 1145 | // if(GasMischanteil < 35) { if(StickGier > 10) StickGier = 10; else if(StickGier < -10) StickGier = -10;}; |
| 1051 | killagreg | 1146 | if(abs(StickGier) > 15) // war 35 |
| 1 | ingob | 1147 | { |
| 921 | hbuss | 1148 | KompassSignalSchlecht = 1000; |
| 1051 | killagreg | 1149 | if(!(EE_Parameter.GlobalConfig & CFG_KOMPASS_FIX)) |
| 1150 | { |
||
| 1151 | NeueKompassRichtungMerken = 1; |
||
| 824 | hbuss | 1152 | }; |
| 1 | ingob | 1153 | } |
| 395 | hbuss | 1154 | tmp_int = (long) EE_Parameter.Gier_P * ((long)StickGier * abs(StickGier)) / 512L; // expo y = ax + bx² |
| 1051 | killagreg | 1155 | tmp_int += (EE_Parameter.Gier_P * StickGier) / 4; |
| 173 | holgerb | 1156 | sollGier = tmp_int; |
| 1051 | killagreg | 1157 | Mess_Integral_Gier -= tmp_int; |
| 395 | hbuss | 1158 | if(Mess_Integral_Gier > 50000) Mess_Integral_Gier = 50000; // begrenzen |
| 1159 | if(Mess_Integral_Gier <-50000) Mess_Integral_Gier =-50000; |
||
| 1051 | killagreg | 1160 | |
| 1161 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1 | ingob | 1162 | // Kompass |
| 1051 | killagreg | 1163 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1175 | hbuss | 1164 | //DebugOut.Analog[16] = KompassSignalSchlecht; |
| 819 | hbuss | 1165 | |
| 1051 | killagreg | 1166 | if(KompassValue && (EE_Parameter.GlobalConfig & CFG_KOMPASS_AKTIV)) |
| 1 | ingob | 1167 | { |
| 819 | hbuss | 1168 | int w,v,r,fehler,korrektur; |
| 1 | ingob | 1169 | w = abs(IntegralNick /512); // mit zunehmender Neigung den Einfluss drosseln |
| 1170 | v = abs(IntegralRoll /512); |
||
| 1171 | if(v > w) w = v; // grösste Neigung ermitteln |
||
| 824 | hbuss | 1172 | korrektur = w / 8 + 1; |
| 921 | hbuss | 1173 | fehler = ((540 + KompassValue - (ErsatzKompass/GIER_GRAD_FAKTOR)) % 360) - 180; |
| 1171 | hbuss | 1174 | if(abs(MesswertGier) > 128) |
| 1036 | hbuss | 1175 | { |
| 1176 | fehler = 0; |
||
| 1051 | killagreg | 1177 | } |
| 1171 | hbuss | 1178 | |
| 1179 | if(NeueKompassRichtungMerken) |
||
| 1180 | { |
||
| 1181 | // ErsatzKompass += (fehler * 32) / korrektur; |
||
| 1182 | // fehler = 0; |
||
| 1183 | // fehler /= 4; |
||
| 1184 | // ErsatzKompass = KompassValue * GIER_GRAD_FAKTOR; |
||
| 1185 | } |
||
| 921 | hbuss | 1186 | if(!KompassSignalSchlecht && w < 25) |
| 1187 | { |
||
| 1188 | GierGyroFehler += fehler; |
||
| 1051 | killagreg | 1189 | if(NeueKompassRichtungMerken) |
| 1190 | { |
||
| 921 | hbuss | 1191 | beeptime = 200; |
| 847 | hbuss | 1192 | // KompassStartwert = KompassValue; |
| 1171 | hbuss | 1193 | ErsatzKompass = KompassValue * GIER_GRAD_FAKTOR; |
| 921 | hbuss | 1194 | KompassStartwert = (ErsatzKompass/GIER_GRAD_FAKTOR); |
| 1195 | NeueKompassRichtungMerken = 0; |
||
| 1196 | } |
||
| 1 | ingob | 1197 | } |
| 824 | hbuss | 1198 | ErsatzKompass += (fehler * 8) / korrektur; |
| 921 | hbuss | 1199 | w = (w * Parameter_KompassWirkung) / 32; // auf die Wirkung normieren |
| 1 | ingob | 1200 | w = Parameter_KompassWirkung - w; // Wirkung ggf drosseln |
| 921 | hbuss | 1201 | if(w >= 0) |
| 1 | ingob | 1202 | { |
| 1051 | killagreg | 1203 | if(!KompassSignalSchlecht) |
| 693 | hbuss | 1204 | { |
| 1051 | killagreg | 1205 | v = 64 + ((MaxStickNick + MaxStickRoll)) / 8; |
| 847 | hbuss | 1206 | r = ((540 + (ErsatzKompass/GIER_GRAD_FAKTOR) - KompassStartwert) % 360) - 180; |
| 1207 | // r = KompassRichtung; |
||
| 819 | hbuss | 1208 | v = (r * w) / v; // nach Kompass ausrichten |
| 1209 | w = 3 * Parameter_KompassWirkung; |
||
| 693 | hbuss | 1210 | if(v > w) v = w; // Begrenzen |
| 1051 | killagreg | 1211 | else |
| 693 | hbuss | 1212 | if(v < -w) v = -w; |
| 1213 | Mess_Integral_Gier += v; |
||
| 1051 | killagreg | 1214 | } |
| 693 | hbuss | 1215 | if(KompassSignalSchlecht) KompassSignalSchlecht--; |
| 1051 | killagreg | 1216 | } |
| 921 | hbuss | 1217 | else KompassSignalSchlecht = 500; // so lange das Signal taub stellen --> ca. 1 sek |
| 1051 | killagreg | 1218 | } |
| 1219 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1 | ingob | 1220 | |
| 1051 | killagreg | 1221 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 1222 | // Debugwerte zuordnen |
| 1051 | killagreg | 1223 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 1224 | if(!TimerWerteausgabe--) |
| 1225 | { |
||
| 395 | hbuss | 1226 | TimerWerteausgabe = 24; |
| 805 | hbuss | 1227 | |
| 1171 | hbuss | 1228 | DebugOut.Analog[0] = IntegralNick / (EE_Parameter.GyroAccFaktor * 4); |
| 1229 | DebugOut.Analog[1] = IntegralRoll / (EE_Parameter.GyroAccFaktor * 4); |
||
| 1230 | DebugOut.Analog[2] = Mittelwert_AccNick / 4; |
||
| 1231 | DebugOut.Analog[3] = Mittelwert_AccRoll / 4; |
||
| 1 | ingob | 1232 | DebugOut.Analog[4] = MesswertGier; |
| 1233 | DebugOut.Analog[5] = HoehenWert; |
||
| 1171 | hbuss | 1234 | DebugOut.Analog[6] = (Mess_Integral_Hoch / 512);//Aktuell_az; |
| 1 | ingob | 1235 | DebugOut.Analog[8] = KompassValue; |
| 297 | holgerb | 1236 | DebugOut.Analog[9] = UBat; |
| 1051 | killagreg | 1237 | DebugOut.Analog[11] = ErsatzKompass / GIER_GRAD_FAKTOR; |
| 297 | holgerb | 1238 | DebugOut.Analog[10] = SenderOkay; |
| 929 | hbuss | 1239 | //DebugOut.Analog[16] = Mittelwert_AccHoch; |
| 1083 | killagreg | 1240 | //DebugOut.Analog[17] = FromNaviCtrl_Value.Distance; |
| 1241 | //DebugOut.Analog[18] = (int)FromNaviCtrl_Value.OsdBar; |
||
| 819 | hbuss | 1242 | DebugOut.Analog[19] = WinkelOut.CalcState; |
| 854 | hbuss | 1243 | DebugOut.Analog[20] = ServoValue; |
| 1171 | hbuss | 1244 | // DebugOut.Analog[24] = MesswertNick/2; |
| 1245 | // DebugOut.Analog[25] = MesswertRoll/2; |
||
| 1173 | hbuss | 1246 | DebugOut.Analog[27] = (int)FromNaviCtrl_Value.Kalman_MaxDrift; |
| 1172 | hbuss | 1247 | // DebugOut.Analog[28] = (int)FromNaviCtrl_Value.Kalman_MaxFusion; |
| 1248 | // DebugOut.Analog[29] = (int)FromNaviCtrl_Value.Kalman_K; |
||
| 1166 | hbuss | 1249 | DebugOut.Analog[30] = GPS_Nick; |
| 720 | ingob | 1250 | DebugOut.Analog[31] = GPS_Roll; |
| 1251 | |||
| 805 | hbuss | 1252 | |
| 1253 | // DebugOut.Analog[19] -= DebugOut.Analog[19]/128; |
||
| 1254 | // if(DebugOut.Analog[19] > 0) DebugOut.Analog[19]--; else DebugOut.Analog[19]++; |
||
| 1255 | |||
| 173 | holgerb | 1256 | /* DebugOut.Analog[16] = motor_rx[0]; |
| 1257 | DebugOut.Analog[17] = motor_rx[1]; |
||
| 1258 | DebugOut.Analog[18] = motor_rx[2]; |
||
| 1259 | DebugOut.Analog[19] = motor_rx[3]; |
||
| 1260 | DebugOut.Analog[20] = motor_rx[0] + motor_rx[1] + motor_rx[2] + motor_rx[3]; |
||
| 1261 | DebugOut.Analog[20] /= 14; |
||
| 1262 | DebugOut.Analog[21] = motor_rx[4]; |
||
| 1263 | DebugOut.Analog[22] = motor_rx[5]; |
||
| 1264 | DebugOut.Analog[23] = motor_rx[6]; |
||
| 1265 | DebugOut.Analog[24] = motor_rx[7]; |
||
| 1266 | DebugOut.Analog[25] = motor_rx[4] + motor_rx[5] + motor_rx[6] + motor_rx[7]; |
||
| 1267 | */ |
||
| 1268 | // DebugOut.Analog[9] = MesswertNick; |
||
| 1 | ingob | 1269 | // DebugOut.Analog[9] = SollHoehe; |
| 1270 | // DebugOut.Analog[10] = Mess_Integral_Gier / 128; |
||
| 1271 | // DebugOut.Analog[11] = KompassStartwert; |
||
| 1051 | killagreg | 1272 | // DebugOut.Analog[10] = Parameter_Gyro_I; |
| 1273 | // DebugOut.Analog[10] = EE_Parameter.Gyro_I; |
||
| 1274 | // DebugOut.Analog[9] = KompassRichtung; |
||
| 1 | ingob | 1275 | // DebugOut.Analog[10] = GasMischanteil; |
| 1276 | // DebugOut.Analog[3] = HoeheD * 32; |
||
| 1277 | // DebugOut.Analog[4] = hoehenregler; |
||
| 1278 | } |
||
| 1279 | |||
| 1051 | killagreg | 1280 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 1281 | // Drehgeschwindigkeit und -winkel zu einem Istwert zusammenfassen |
| 1051 | killagreg | 1282 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1153 | hbuss | 1283 | if(TrichterFlug) { SummeRoll = 0; SummeNick = 0;}; |
| 604 | hbuss | 1284 | |
| 1171 | hbuss | 1285 | if(!Looping_Nick) IntegralNickMalFaktor = (IntegralNick * IntegralFaktor) / (44000 / STICK_GAIN); else IntegralNickMalFaktor = 0; |
| 1286 | if(!Looping_Roll) IntegralRollMalFaktor = (IntegralRoll * IntegralFaktor) / (44000 / STICK_GAIN); else IntegralRollMalFaktor = 0; |
||
| 1153 | hbuss | 1287 | |
| 1167 | hbuss | 1288 | #define TRIM_MAX 200 |
| 1166 | hbuss | 1289 | if(TrimNick > TRIM_MAX) TrimNick = TRIM_MAX; else if(TrimNick <-TRIM_MAX) TrimNick =-TRIM_MAX; |
| 1290 | if(TrimRoll > TRIM_MAX) TrimRoll = TRIM_MAX; else if(TrimRoll <-TRIM_MAX) TrimRoll =-TRIM_MAX; |
||
| 1153 | hbuss | 1291 | |
| 1166 | hbuss | 1292 | { |
| 1293 | MesswertNick = IntegralNickMalFaktor + (long)((long)MesswertNick * GyroFaktor + (long)TrimNick * 128L) / (256L / STICK_GAIN); |
||
| 1294 | MesswertRoll = IntegralRollMalFaktor + (long)((long)MesswertRoll * GyroFaktor + (long)TrimRoll * 128L) / (256L / STICK_GAIN); |
||
| 1295 | } |
||
| 1296 | |||
| 1297 | #ifndef QUADRO |
||
| 1153 | hbuss | 1298 | MesswertGier = (long)(MesswertGier * 4 * (long)GyroFaktor) / (256L / STICK_GAIN) + (long)(Integral_Gier * IntegralFaktor) / (4 * (44000 / STICK_GAIN)); |
| 1111 | hbuss | 1299 | #else |
| 1153 | hbuss | 1300 | MesswertGier = (long)(MesswertGier * 2 * (long)GyroFaktor) / (256L / STICK_GAIN) + (long)(Integral_Gier * IntegralFaktor) / (2 * (44000 / STICK_GAIN)); |
| 1301 | #endif |
||
| 1 | ingob | 1302 | |
| 1303 | // Maximalwerte abfangen |
||
| 1153 | hbuss | 1304 | // #define MAX_SENSOR (4096*STICK_GAIN) |
| 1305 | #define MAX_SENSOR (4096*4) |
||
| 1306 | if(MesswertNick > MAX_SENSOR) MesswertNick = MAX_SENSOR; |
||
| 1 | ingob | 1307 | if(MesswertNick < -MAX_SENSOR) MesswertNick = -MAX_SENSOR; |
| 1308 | if(MesswertRoll > MAX_SENSOR) MesswertRoll = MAX_SENSOR; |
||
| 1309 | if(MesswertRoll < -MAX_SENSOR) MesswertRoll = -MAX_SENSOR; |
||
| 1310 | if(MesswertGier > MAX_SENSOR) MesswertGier = MAX_SENSOR; |
||
| 1311 | if(MesswertGier < -MAX_SENSOR) MesswertGier = -MAX_SENSOR; |
||
| 1312 | |||
| 1051 | killagreg | 1313 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1210 | hbuss | 1314 | // all BL-Ctrl connected? |
| 1315 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1316 | if(MissingMotor) if(modell_fliegt > 1 && modell_fliegt < 50 && GasMischanteil > 0) |
||
| 1317 | { |
||
| 1318 | modell_fliegt = 1; |
||
| 1319 | GasMischanteil = MIN_GAS; |
||
| 1320 | } |
||
| 1321 | |||
| 1322 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1 | ingob | 1323 | // Höhenregelung |
| 1324 | // Die Höhenregelung schwächt lediglich das Gas ab, erhöht es allerdings nicht |
||
| 1051 | killagreg | 1325 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 855 | hbuss | 1326 | GasMischanteil *= STICK_GAIN; |
| 1 | ingob | 1327 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG)) // Höhenregelung |
| 1328 | { |
||
| 1329 | int tmp_int; |
||
| 1036 | hbuss | 1330 | static char delay = 100; |
| 1 | ingob | 1331 | if(EE_Parameter.GlobalConfig & CFG_HOEHEN_SCHALTER) // Regler wird über Schalter gesteuert |
| 1332 | { |
||
| 1036 | hbuss | 1333 | if(((EE_Parameter.BitConfig & CFG_HIGHT_3SWITCH) && ((Parameter_MaxHoehe > 80) && (Parameter_MaxHoehe < 140))) || |
| 993 | hbuss | 1334 | (!(EE_Parameter.BitConfig & CFG_HIGHT_3SWITCH) && (Parameter_MaxHoehe < 50))) |
| 1 | ingob | 1335 | { |
| 1036 | hbuss | 1336 | if(!delay--) |
| 1337 | { |
||
| 1051 | killagreg | 1338 | if(MessLuftdruck > 1000) |
| 1036 | hbuss | 1339 | { |
| 1340 | ExpandBaro -= 10; |
||
| 1051 | killagreg | 1341 | OCR0A = DruckOffsetSetting - ExpandBaro; |
| 1036 | hbuss | 1342 | beeptime = 300; |
| 1343 | delay = 250; |
||
| 1344 | } |
||
| 1345 | else |
||
| 1051 | killagreg | 1346 | if(MessLuftdruck < 100) |
| 1036 | hbuss | 1347 | { |
| 1348 | ExpandBaro += 10; |
||
| 1051 | killagreg | 1349 | OCR0A = DruckOffsetSetting - ExpandBaro; |
| 1036 | hbuss | 1350 | beeptime = 300; |
| 1351 | delay = 250; |
||
| 1352 | } |
||
| 1353 | else |
||
| 1051 | killagreg | 1354 | { |
| 1036 | hbuss | 1355 | SollHoehe = HoehenWert - 20; // Parameter_MaxHoehe ist der PPM-Wert des Schalters |
| 1356 | HoehenReglerAktiv = 0; |
||
| 1357 | delay = 1; |
||
| 1358 | } |
||
| 1051 | killagreg | 1359 | } |
| 1 | ingob | 1360 | } |
| 1051 | killagreg | 1361 | else |
| 1362 | { |
||
| 1036 | hbuss | 1363 | HoehenReglerAktiv = 1; |
| 1364 | delay = 200; |
||
| 1051 | killagreg | 1365 | } |
| 1 | ingob | 1366 | } |
| 1051 | killagreg | 1367 | else |
| 1 | ingob | 1368 | { |
| 492 | hbuss | 1369 | SollHoehe = ((int) ExternHoehenValue + (int) Parameter_MaxHoehe) * (int)EE_Parameter.Hoehe_Verstaerkung - 20; |
| 1 | ingob | 1370 | HoehenReglerAktiv = 1; |
| 1371 | } |
||
| 1372 | |||
| 1373 | if(Notlandung) SollHoehe = 0; |
||
| 1374 | h = HoehenWert; |
||
| 1375 | if((h > SollHoehe) && HoehenReglerAktiv) // zu hoch --> drosseln |
||
| 1051 | killagreg | 1376 | { |
| 855 | hbuss | 1377 | h = ((h - SollHoehe) * (int) Parameter_Hoehe_P) / (16 / STICK_GAIN); // Differenz bestimmen --> P-Anteil |
| 1 | ingob | 1378 | h = GasMischanteil - h; // vom Gas abziehen |
| 871 | hbuss | 1379 | // h -= (HoeheD * Parameter_Luftdruck_D)/(8/STICK_GAIN); // D-Anteil |
| 1380 | h -= (HoeheD)/(8/STICK_GAIN); // D-Anteil |
||
| 1381 | tmp_int = ((Mess_Integral_Hoch / 128) * (signed long) Parameter_Hoehe_ACC_Wirkung) / (128 / STICK_GAIN); |
||
| 1382 | if(tmp_int > 70*STICK_GAIN) tmp_int = 70*STICK_GAIN; |
||
| 1383 | else if(tmp_int < -(70*STICK_GAIN)) tmp_int = -(70*STICK_GAIN); |
||
| 1 | ingob | 1384 | h -= tmp_int; |
| 1051 | killagreg | 1385 | hoehenregler = (hoehenregler*15 + h) / 16; |
| 855 | hbuss | 1386 | if(hoehenregler < EE_Parameter.Hoehe_MinGas * STICK_GAIN) // nicht unter MIN |
| 1 | ingob | 1387 | { |
| 855 | hbuss | 1388 | if(GasMischanteil >= EE_Parameter.Hoehe_MinGas * STICK_GAIN) hoehenregler = EE_Parameter.Hoehe_MinGas * STICK_GAIN; |
| 1389 | if(GasMischanteil < EE_Parameter.Hoehe_MinGas * STICK_GAIN) hoehenregler = GasMischanteil; |
||
| 1051 | killagreg | 1390 | } |
| 1 | ingob | 1391 | if(hoehenregler > GasMischanteil) hoehenregler = GasMischanteil; // nicht mehr als Gas |
| 1392 | GasMischanteil = hoehenregler; |
||
| 1051 | killagreg | 1393 | } |
| 1 | ingob | 1394 | } |
| 855 | hbuss | 1395 | if(GasMischanteil > (MAX_GAS - 20) * STICK_GAIN) GasMischanteil = (MAX_GAS - 20) * STICK_GAIN; |
| 1111 | hbuss | 1396 | |
| 1051 | killagreg | 1397 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 1398 | // + Mischer und PI-Regler |
| 1051 | killagreg | 1399 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 173 | holgerb | 1400 | DebugOut.Analog[7] = GasMischanteil; |
| 1051 | killagreg | 1401 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 1402 | // Gier-Anteil |
| 1051 | killagreg | 1403 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 188 | holgerb | 1404 | #define MUL_G 1.0 |
| 855 | hbuss | 1405 | GierMischanteil = MesswertGier - sollGier * STICK_GAIN; // Regler für Gier |
| 604 | hbuss | 1406 | // GierMischanteil = 0; |
| 855 | hbuss | 1407 | #define MIN_GIERGAS (40*STICK_GAIN) // unter diesem Gaswert trotzdem Gieren |
| 693 | hbuss | 1408 | if(GasMischanteil > MIN_GIERGAS) |
| 1409 | { |
||
| 1051 | killagreg | 1410 | if(GierMischanteil > (GasMischanteil / 2)) GierMischanteil = GasMischanteil / 2; |
| 1411 | if(GierMischanteil < -(GasMischanteil / 2)) GierMischanteil = -(GasMischanteil / 2); |
||
| 693 | hbuss | 1412 | } |
| 1051 | killagreg | 1413 | else |
| 693 | hbuss | 1414 | { |
| 1051 | killagreg | 1415 | if(GierMischanteil > (MIN_GIERGAS / 2)) GierMischanteil = MIN_GIERGAS / 2; |
| 1416 | if(GierMischanteil < -(MIN_GIERGAS / 2)) GierMischanteil = -(MIN_GIERGAS / 2); |
||
| 693 | hbuss | 1417 | } |
| 855 | hbuss | 1418 | tmp_int = MAX_GAS*STICK_GAIN; |
| 1051 | killagreg | 1419 | if(GierMischanteil > ((tmp_int - GasMischanteil))) GierMischanteil = ((tmp_int - GasMischanteil)); |
| 855 | hbuss | 1420 | if(GierMischanteil < -((tmp_int - GasMischanteil))) GierMischanteil = -((tmp_int - GasMischanteil)); |
| 513 | hbuss | 1421 | |
| 1051 | killagreg | 1422 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 1423 | // Nick-Achse |
| 1051 | killagreg | 1424 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 723 | hbuss | 1425 | DiffNick = MesswertNick - StickNick; // Differenz bestimmen |
| 1153 | hbuss | 1426 | if(IntegralFaktor) SummeNick += IntegralNickMalFaktor - StickNick; // I-Anteil bei Winkelregelung |
| 1051 | killagreg | 1427 | else SummeNick += DiffNick; // I-Anteil bei HH |
| 855 | hbuss | 1428 | if(SummeNick > (STICK_GAIN * 16000L)) SummeNick = (STICK_GAIN * 16000L); |
| 1429 | if(SummeNick < -(16000L * STICK_GAIN)) SummeNick = -(16000L * STICK_GAIN); |
||
| 1153 | hbuss | 1430 | pd_ergebnis_nick = DiffNick + SummeNick / Ki; // PI-Regler für Nick |
| 1 | ingob | 1431 | // Motor Vorn |
| 499 | hbuss | 1432 | tmp_int = (long)((long)Parameter_DynamicStability * (long)(GasMischanteil + abs(GierMischanteil)/2)) / 64; |
| 1153 | hbuss | 1433 | if(pd_ergebnis_nick > tmp_int) pd_ergebnis_nick = tmp_int; |
| 1434 | if(pd_ergebnis_nick < -tmp_int) pd_ergebnis_nick = -tmp_int; |
||
| 173 | holgerb | 1435 | |
| 1153 | hbuss | 1436 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1437 | // Roll-Achse |
||
| 1438 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1439 | DiffRoll = MesswertRoll - StickRoll; // Differenz bestimmen |
||
| 1440 | if(IntegralFaktor) SummeRoll += IntegralRollMalFaktor - StickRoll;// I-Anteil bei Winkelregelung |
||
| 1441 | else SummeRoll += DiffRoll; // I-Anteil bei HH |
||
| 1442 | if(SummeRoll > (STICK_GAIN * 16000L)) SummeRoll = (STICK_GAIN * 16000L); |
||
| 1443 | if(SummeRoll < -(16000L * STICK_GAIN)) SummeRoll = -(16000L * STICK_GAIN); |
||
| 1444 | pd_ergebnis_roll = DiffRoll + SummeRoll / Ki; // PI-Regler für Roll |
||
| 1445 | tmp_int = (long)((long)Parameter_DynamicStability * (long)(GasMischanteil + abs(GierMischanteil)/2)) / 64; |
||
| 1446 | if(pd_ergebnis_roll > tmp_int) pd_ergebnis_roll = tmp_int; |
||
| 1447 | if(pd_ergebnis_roll < -tmp_int) pd_ergebnis_roll = -tmp_int; |
||
| 1448 | |||
| 1449 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1209 | hbuss | 1450 | // Universal Mixer |
| 1155 | hbuss | 1451 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1209 | hbuss | 1452 | for(i=0; i<MAX_MOTORS; i++) |
| 1453 | { |
||
| 1454 | signed int tmp_int; |
||
| 1455 | if(Mixer.Motor[i][0] > 0) |
||
| 1456 | { |
||
| 1457 | tmp_int = ((long)GasMischanteil * Mixer.Motor[i][0]) / 64L; |
||
| 1458 | tmp_int += ((long)pd_ergebnis_nick * Mixer.Motor[i][1]) / 64L; |
||
| 1459 | tmp_int += ((long)pd_ergebnis_roll * Mixer.Motor[i][2]) / 64L; |
||
| 1460 | tmp_int += ((long)GierMischanteil * Mixer.Motor[i][3]) / 64L; |
||
| 1461 | tmp_motorwert[i] = MotorSmoothing(tmp_int,tmp_motorwert[i]); // Filter |
||
| 1462 | tmp_int = tmp_motorwert[i] / STICK_GAIN; |
||
| 1463 | CHECK_MIN_MAX(tmp_int,MIN_GAS,MAX_GAS); |
||
| 1464 | Motor[i] = tmp_int; |
||
| 1465 | } |
||
| 1466 | else Motor[i] = 0; |
||
| 1467 | } |
||
| 1167 | hbuss | 1468 | /* |
| 1153 | hbuss | 1469 | if(Poti1 > 20) Motor1 = 0; |
| 1470 | if(Poti1 > 90) Motor6 = 0; |
||
| 1471 | if(Poti1 > 140) Motor2 = 0; |
||
| 1175 | hbuss | 1472 | //if(Poti1 > 200) Motor7 = 0; |
| 1167 | hbuss | 1473 | */ |
| 1111 | hbuss | 1474 | } |