Rev 1596 | Details | Compare with Previous | Last modification | View Log | RSS feed
| Rev | Author | Line No. | Line |
|---|---|---|---|
| 1 | ingob | 1 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1338 | ingob | 2 | // + Copyright (c) Holger Buss, Ingo Busker |
| 1 | ingob | 3 | // + only for non-profit use |
| 4 | // + www.MikroKopter.com |
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| 1356 | hbuss | 5 | // + porting the sources to other systems or using the software on other systems (except hardware from www.mikrokopter.de) is not allowed |
| 1 | ingob | 6 | // + see the File "License.txt" for further Informations |
| 7 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
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| 8 | |||
| 9 | #include "main.h" |
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| 10 | volatile int Aktuell_Nick,Aktuell_Roll,Aktuell_Gier,Aktuell_ax, Aktuell_ay,Aktuell_az, UBat = 100; |
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| 1166 | hbuss | 11 | volatile int AdWertNickFilter = 0, AdWertRollFilter = 0, AdWertGierFilter = 0; |
| 12 | volatile int HiResNick = 2500, HiResRoll = 2500; |
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| 380 | hbuss | 13 | volatile int AdWertNick = 0, AdWertRoll = 0, AdWertGier = 0; |
| 14 | volatile int AdWertAccRoll = 0,AdWertAccNick = 0,AdWertAccHoch = 0; |
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| 1166 | hbuss | 15 | volatile char messanzahl_AccHoch = 0; |
| 1 | ingob | 16 | volatile long Luftdruck = 32000; |
| 1322 | hbuss | 17 | volatile long SummenHoehe = 0; |
| 1 | ingob | 18 | volatile int StartLuftdruck; |
| 19 | volatile unsigned int MessLuftdruck = 1023; |
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| 20 | unsigned char DruckOffsetSetting; |
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| 1036 | hbuss | 21 | signed char ExpandBaro = 0; |
| 1253 | killagreg | 22 | volatile int VarioMeter = 0; |
| 1 | ingob | 23 | volatile unsigned int ZaehlMessungen = 0; |
| 918 | hbuss | 24 | unsigned char AnalogOffsetNick = 115,AnalogOffsetRoll = 115,AnalogOffsetGier = 115; |
| 25 | unsigned char GyroDefektN = 0,GyroDefektR = 0,GyroDefektG = 0; |
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| 1168 | hbuss | 26 | volatile unsigned char AdReady = 1; |
| 1 | ingob | 27 | //####################################################################################### |
| 28 | // |
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| 29 | void ADC_Init(void) |
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| 30 | //####################################################################################### |
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| 1246 | killagreg | 31 | { |
| 1 | ingob | 32 | ADMUX = 0;//Referenz ist extern |
| 1155 | hbuss | 33 | ANALOG_ON; |
| 1 | ingob | 34 | } |
| 35 | |||
| 1352 | hbuss | 36 | #define DESIRED_H_ADC 800 |
| 1322 | hbuss | 37 | |
| 1 | ingob | 38 | void SucheLuftruckOffset(void) |
| 39 | { |
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| 40 | unsigned int off; |
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| 173 | holgerb | 41 | off = eeprom_read_byte(&EEPromArray[EEPROM_ADR_LAST_OFFSET]); |
| 42 | if(off > 20) off -= 10; |
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| 43 | OCR0A = off; |
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| 1036 | hbuss | 44 | ExpandBaro = 0; |
| 380 | hbuss | 45 | Delay_ms_Mess(100); |
| 1322 | hbuss | 46 | if(MessLuftdruck < DESIRED_H_ADC) off = 0; |
| 173 | holgerb | 47 | for(; off < 250;off++) |
| 1 | ingob | 48 | { |
| 49 | OCR0A = off; |
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| 380 | hbuss | 50 | Delay_ms_Mess(50); |
| 1246 | killagreg | 51 | printf("."); |
| 1322 | hbuss | 52 | if(MessLuftdruck < DESIRED_H_ADC) break; |
| 1 | ingob | 53 | } |
| 173 | holgerb | 54 | eeprom_write_byte(&EEPromArray[EEPROM_ADR_LAST_OFFSET], off); |
| 55 | DruckOffsetSetting = off; |
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| 380 | hbuss | 56 | Delay_ms_Mess(300); |
| 1 | ingob | 57 | } |
| 58 | |||
| 918 | hbuss | 59 | void SucheGyroOffset(void) |
| 60 | { |
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| 61 | unsigned char i, ready = 0; |
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| 1219 | hbuss | 62 | int timeout; |
| 918 | hbuss | 63 | GyroDefektN = 0; GyroDefektR = 0; GyroDefektG = 0; |
| 1219 | hbuss | 64 | timeout = SetDelay(2000); |
| 918 | hbuss | 65 | for(i=140; i != 0; i--) |
| 66 | { |
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| 921 | hbuss | 67 | if(ready == 3 && i > 10) i = 9; |
| 918 | hbuss | 68 | ready = 0; |
| 69 | if(AdWertNick < 1020) AnalogOffsetNick--; else if(AdWertNick > 1030) AnalogOffsetNick++; else ready++; |
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| 70 | if(AdWertRoll < 1020) AnalogOffsetRoll--; else if(AdWertRoll > 1030) AnalogOffsetRoll++; else ready++; |
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| 71 | if(AdWertGier < 1020) AnalogOffsetGier--; else if(AdWertGier > 1030) AnalogOffsetGier++; else ready++; |
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| 1246 | killagreg | 72 | twi_state = 8; |
| 73 | i2c_start(); |
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| 74 | if(AnalogOffsetNick < 10) { GyroDefektN = 1; AnalogOffsetNick = 10;}; if(AnalogOffsetNick > 245) { GyroDefektN = 1; AnalogOffsetNick = 245;}; |
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| 75 | if(AnalogOffsetRoll < 10) { GyroDefektR = 1; AnalogOffsetRoll = 10;}; if(AnalogOffsetRoll > 245) { GyroDefektR = 1; AnalogOffsetRoll = 245;}; |
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| 76 | if(AnalogOffsetGier < 10) { GyroDefektG = 1; AnalogOffsetGier = 10;}; if(AnalogOffsetGier > 245) { GyroDefektG = 1; AnalogOffsetGier = 245;}; |
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| 1219 | hbuss | 77 | while(twi_state) if(CheckDelay(timeout)) {printf("\n\r DAC or I2C ERROR! Check I2C, 3Vref, DAC and BL-Ctrl"); break;} |
| 1253 | killagreg | 78 | AdReady = 0; |
| 918 | hbuss | 79 | ANALOG_ON; |
| 1253 | killagreg | 80 | while(!AdReady); |
| 1246 | killagreg | 81 | if(i<10) Delay_ms_Mess(10); |
| 918 | hbuss | 82 | } |
| 1246 | killagreg | 83 | Delay_ms_Mess(70); |
| 84 | } |
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| 1 | ingob | 85 | |
| 1171 | hbuss | 86 | /* |
| 87 | |||
| 88 | 1 r |
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| 1246 | killagreg | 89 | 2 g |
| 1171 | hbuss | 90 | 3 y |
| 91 | 4 x |
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| 92 | 5 n |
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| 93 | 6 r |
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| 94 | 7 u |
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| 95 | 8 z |
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| 96 | 9 L |
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| 1246 | killagreg | 97 | 10 n |
| 1171 | hbuss | 98 | 11 r |
| 99 | 12 g |
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| 100 | 13 y |
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| 101 | 14 x |
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| 102 | 15 n |
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| 103 | 16 r |
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| 104 | 17 L |
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| 105 | */ |
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| 106 | |||
| 1 | ingob | 107 | //####################################################################################### |
| 108 | // |
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| 1561 | killagreg | 109 | ISR(ADC_vect) |
| 1 | ingob | 110 | //####################################################################################### |
| 111 | { |
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| 112 | static unsigned char kanal=0,state = 0; |
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| 1246 | killagreg | 113 | static signed int gier1, roll1, nick1, nick_filter, roll_filter; |
| 1171 | hbuss | 114 | static signed int accy, accx; |
| 1253 | killagreg | 115 | |
| 116 | static long tmpLuftdruck = 0; |
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| 117 | static char messanzahl_Druck = 0; |
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| 1171 | hbuss | 118 | switch(state++) |
| 119 | { |
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| 120 | case 0: |
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| 121 | nick1 = ADC; |
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| 122 | kanal = AD_ROLL; |
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| 123 | break; |
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| 124 | case 1: |
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| 125 | roll1 = ADC; |
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| 126 | kanal = AD_GIER; |
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| 127 | break; |
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| 128 | case 2: |
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| 129 | gier1 = ADC; |
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| 130 | kanal = AD_ACC_Y; |
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| 131 | break; |
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| 132 | case 3: |
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| 133 | Aktuell_ay = NeutralAccY - ADC; |
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| 134 | accy = Aktuell_ay; |
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| 135 | kanal = AD_ACC_X; |
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| 136 | break; |
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| 137 | case 4: |
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| 138 | Aktuell_ax = ADC - NeutralAccX; |
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| 139 | accx = Aktuell_ax; |
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| 140 | kanal = AD_NICK; |
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| 141 | break; |
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| 142 | case 5: |
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| 143 | nick1 += ADC; |
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| 144 | kanal = AD_ROLL; |
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| 145 | break; |
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| 146 | case 6: |
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| 147 | roll1 += ADC; |
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| 148 | kanal = AD_UBAT; |
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| 149 | break; |
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| 150 | case 7: |
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| 151 | UBat = (3 * UBat + ADC / 3) / 4; |
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| 152 | kanal = AD_ACC_Z; |
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| 153 | break; |
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| 154 | case 8: |
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| 155 | AdWertAccHoch = (signed int) ADC - NeutralAccZ; |
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| 1604 | MartinR | 156 | /* // MartinR: deaktiviert |
| 1246 | killagreg | 157 | if(AdWertAccHoch > 1) |
| 1171 | hbuss | 158 | { |
| 1246 | killagreg | 159 | if(NeutralAccZ < 750) |
| 1171 | hbuss | 160 | { |
| 1246 | killagreg | 161 | NeutralAccZ += 0.02; |
| 162 | if(modell_fliegt < 500) NeutralAccZ += 0.1; |
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| 163 | } |
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| 164 | } |
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| 1171 | hbuss | 165 | else if(AdWertAccHoch < -1) |
| 166 | { |
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| 1246 | killagreg | 167 | if(NeutralAccZ > 550) |
| 1171 | hbuss | 168 | { |
| 169 | NeutralAccZ-= 0.02; |
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| 1246 | killagreg | 170 | if(modell_fliegt < 500) NeutralAccZ -= 0.1; |
| 171 | } |
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| 172 | } |
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| 1604 | MartinR | 173 | */ // MartinR: deaktiviert Ende |
| 174 | |||
| 1171 | hbuss | 175 | messanzahl_AccHoch = 1; |
| 176 | Aktuell_az = ADC; |
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| 177 | Mess_Integral_Hoch += AdWertAccHoch; // Integrieren |
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| 178 | Mess_Integral_Hoch -= Mess_Integral_Hoch / 1024; // dämfen |
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| 179 | kanal = AD_DRUCK; |
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| 180 | break; |
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| 181 | // "case 8:" fehlt hier absichtlich |
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| 182 | case 10: |
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| 183 | nick1 += ADC; |
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| 184 | kanal = AD_ROLL; |
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| 185 | break; |
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| 186 | case 11: |
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| 187 | roll1 += ADC; |
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| 188 | kanal = AD_GIER; |
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| 189 | break; |
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| 190 | case 12: |
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| 191 | if(PlatinenVersion == 10) AdWertGier = (ADC + gier1 + 1) / 2; |
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| 1246 | killagreg | 192 | else |
| 1171 | hbuss | 193 | if(PlatinenVersion == 20) AdWertGier = 2047 - (ADC + gier1); |
| 194 | else AdWertGier = (ADC + gier1); |
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| 195 | kanal = AD_ACC_Y; |
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| 196 | break; |
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| 197 | case 13: |
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| 198 | Aktuell_ay = NeutralAccY - ADC; |
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| 199 | AdWertAccRoll = (Aktuell_ay + accy); |
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| 200 | kanal = AD_ACC_X; |
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| 201 | break; |
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| 202 | case 14: |
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| 203 | Aktuell_ax = ADC - NeutralAccX; |
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| 204 | AdWertAccNick = (Aktuell_ax + accx); |
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| 205 | kanal = AD_NICK; |
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| 206 | break; |
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| 207 | case 15: |
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| 208 | nick1 += ADC; |
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| 1173 | hbuss | 209 | if(PlatinenVersion == 10) nick1 *= 2; else nick1 *= 4; |
| 210 | AdWertNick = nick1 / 8; |
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| 211 | nick_filter = (nick_filter + nick1) / 2; |
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| 212 | HiResNick = nick_filter - AdNeutralNick; |
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| 1171 | hbuss | 213 | AdWertNickFilter = (AdWertNickFilter + HiResNick) / 2; |
| 214 | kanal = AD_ROLL; |
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| 215 | break; |
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| 216 | case 16: |
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| 217 | roll1 += ADC; |
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| 1173 | hbuss | 218 | if(PlatinenVersion == 10) roll1 *= 2; else roll1 *= 4; |
| 219 | AdWertRoll = roll1 / 8; |
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| 220 | roll_filter = (roll_filter + roll1) / 2; |
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| 221 | HiResRoll = roll_filter - AdNeutralRoll; |
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| 1171 | hbuss | 222 | AdWertRollFilter = (AdWertRollFilter + HiResRoll) / 2; |
| 223 | kanal = AD_DRUCK; |
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| 224 | break; |
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| 225 | case 17: |
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| 226 | state = 0; |
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| 227 | AdReady = 1; |
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| 228 | ZaehlMessungen++; |
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| 229 | // "break" fehlt hier absichtlich |
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| 230 | case 9: |
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| 1253 | killagreg | 231 | MessLuftdruck = ADC; |
| 232 | tmpLuftdruck += MessLuftdruck; |
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| 233 | if(++messanzahl_Druck >= 18) |
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| 234 | { |
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| 1266 | killagreg | 235 | Luftdruck = (7 * Luftdruck + tmpLuftdruck - (18 * 523) * (long)ExpandBaro + 4) / 8; // -523.19 counts per 10 counts offset step |
| 1253 | killagreg | 236 | HoehenWert = StartLuftdruck - Luftdruck; |
| 1272 | hbuss | 237 | SummenHoehe -= SummenHoehe/SM_FILTER; |
| 1253 | killagreg | 238 | SummenHoehe += HoehenWert; |
| 1272 | hbuss | 239 | VarioMeter = (15 * VarioMeter + 8 * (int)(HoehenWert - SummenHoehe/SM_FILTER))/16; |
| 240 | tmpLuftdruck /= 2; |
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| 241 | messanzahl_Druck = 18/2; |
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| 1253 | killagreg | 242 | } |
| 1171 | hbuss | 243 | kanal = AD_NICK; |
| 244 | break; |
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| 1246 | killagreg | 245 | default: |
| 1171 | hbuss | 246 | kanal = 0; state = 0; kanal = AD_NICK; |
| 247 | break; |
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| 1246 | killagreg | 248 | } |
| 1171 | hbuss | 249 | ADMUX = kanal; |
| 250 | if(state != 0) ANALOG_ON; |
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| 1320 | hbuss | 251 | |
| 1171 | hbuss | 252 | } |
| 253 | |||
| 254 | |||
| 255 | |||
| 256 | /* |
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| 257 | //####################################################################################### |
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| 258 | // |
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| 259 | SIGNAL(SIG_ADC) |
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| 260 | //####################################################################################### |
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| 261 | { |
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| 262 | static unsigned char kanal=0,state = 0; |
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| 1166 | hbuss | 263 | static signed int gier1, roll1, nick1; |
| 1246 | killagreg | 264 | static signed long nick_filter, roll_filter; |
| 1166 | hbuss | 265 | static signed int accy, accx; |
| 266 | switch(state++) |
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| 267 | { |
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| 268 | case 0: |
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| 269 | nick1 = ADC; |
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| 270 | kanal = AD_ROLL; |
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| 271 | break; |
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| 272 | case 1: |
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| 273 | roll1 = ADC; |
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| 274 | kanal = AD_GIER; |
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| 275 | break; |
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| 276 | case 2: |
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| 277 | gier1 = ADC; |
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| 278 | kanal = AD_ACC_Y; |
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| 279 | break; |
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| 280 | case 3: |
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| 281 | Aktuell_ay = NeutralAccY - ADC; |
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| 282 | accy = Aktuell_ay; |
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| 283 | kanal = AD_NICK; |
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| 284 | break; |
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| 285 | case 4: |
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| 286 | nick1 += ADC; |
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| 287 | kanal = AD_ROLL; |
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| 288 | break; |
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| 289 | case 5: |
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| 290 | roll1 += ADC; |
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| 291 | kanal = AD_ACC_Z; |
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| 292 | break; |
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| 293 | case 6: |
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| 294 | AdWertAccHoch = (signed int) ADC - NeutralAccZ; |
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| 1246 | killagreg | 295 | if(AdWertAccHoch > 1) |
| 1166 | hbuss | 296 | { |
| 1246 | killagreg | 297 | if(NeutralAccZ < 750) |
| 1166 | hbuss | 298 | { |
| 1246 | killagreg | 299 | NeutralAccZ += 0.02; |
| 300 | if(modell_fliegt < 500) NeutralAccZ += 0.1; |
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| 301 | } |
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| 302 | } |
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| 1166 | hbuss | 303 | else if(AdWertAccHoch < -1) |
| 304 | { |
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| 1246 | killagreg | 305 | if(NeutralAccZ > 550) |
| 1166 | hbuss | 306 | { |
| 307 | NeutralAccZ-= 0.02; |
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| 1246 | killagreg | 308 | if(modell_fliegt < 500) NeutralAccZ -= 0.1; |
| 309 | } |
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| 310 | } |
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| 1166 | hbuss | 311 | messanzahl_AccHoch = 1; |
| 312 | Aktuell_az = ADC; |
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| 313 | Mess_Integral_Hoch += AdWertAccHoch; // Integrieren |
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| 314 | Mess_Integral_Hoch -= Mess_Integral_Hoch / 1024; // dämfen |
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| 315 | kanal = AD_NICK; |
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| 316 | break; |
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| 317 | case 7: |
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| 318 | nick1 += ADC; |
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| 319 | kanal = AD_ROLL; |
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| 320 | break; |
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| 321 | case 8: |
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| 322 | roll1 += ADC; |
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| 323 | kanal = AD_ACC_X; |
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| 324 | break; |
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| 325 | case 9: |
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| 326 | Aktuell_ax = ADC - NeutralAccX; |
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| 327 | accx = Aktuell_ax; |
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| 328 | kanal = AD_GIER; |
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| 329 | break; |
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| 330 | case 10: |
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| 331 | gier1 += ADC; |
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| 332 | kanal = AD_NICK; |
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| 333 | break; |
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| 334 | case 11: |
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| 335 | nick1 += ADC; |
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| 336 | kanal = AD_ROLL; |
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| 337 | break; |
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| 338 | case 12: |
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| 339 | roll1 += ADC; |
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| 340 | kanal = AD_UBAT; |
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| 341 | break; |
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| 342 | case 13: |
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| 343 | UBat = (3 * UBat + ADC / 3) / 4;//(UBat + ((ADC * 39) / 256) + 19) / 2; |
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| 344 | kanal = AD_ACC_Y; |
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| 345 | break; |
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| 346 | case 14: |
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| 347 | Aktuell_ay = NeutralAccY - ADC; |
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| 348 | accy += Aktuell_ay; |
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| 349 | kanal = AD_NICK; |
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| 350 | break; |
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| 351 | case 15: |
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| 352 | nick1 += ADC; |
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| 353 | kanal = AD_ROLL; |
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| 354 | break; |
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| 355 | case 16: |
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| 356 | roll1 += ADC; |
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| 357 | kanal = AD_ACC_X; |
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| 358 | break; |
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| 359 | case 17: |
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| 360 | Aktuell_ax = ADC - NeutralAccX; |
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| 361 | accx += Aktuell_ax; |
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| 362 | kanal = AD_NICK; |
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| 363 | break; |
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| 364 | case 18: |
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| 365 | nick1 += ADC; |
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| 366 | kanal = AD_ROLL; |
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| 367 | break; |
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| 368 | case 19: |
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| 369 | roll1 += ADC; |
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| 370 | kanal = AD_GIER; |
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| 371 | break; |
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| 372 | case 20: |
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| 373 | gier1 += ADC; |
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| 374 | kanal = AD_ACC_Y; |
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| 375 | break; |
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| 376 | case 21: |
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| 377 | Aktuell_ay = NeutralAccY - ADC; |
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| 378 | accy += Aktuell_ay; |
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| 379 | kanal = AD_NICK; |
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| 380 | break; |
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| 381 | case 22: |
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| 382 | nick1 += ADC; |
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| 383 | kanal = AD_ROLL; |
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| 384 | break; |
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| 385 | case 23: |
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| 386 | roll1 += ADC; |
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| 387 | kanal = AD_DRUCK; |
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| 388 | break; |
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| 389 | case 24: |
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| 390 | tmpLuftdruck += ADC; |
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| 1246 | killagreg | 391 | if(++messanzahl_Druck >= 5) |
| 1166 | hbuss | 392 | { |
| 393 | MessLuftdruck = ADC; |
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| 394 | messanzahl_Druck = 0; |
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| 1167 | hbuss | 395 | HoeheD = (7 * HoeheD + (int) Parameter_Luftdruck_D * (int)(255 * ExpandBaro + StartLuftdruck - tmpLuftdruck - HoehenWert)) / 8; // D-Anteil = neuerWert - AlterWert |
| 1166 | hbuss | 396 | Luftdruck = (tmpLuftdruck + 3 * Luftdruck) / 4; |
| 397 | HoehenWert = 255 * ExpandBaro + StartLuftdruck - Luftdruck; |
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| 398 | tmpLuftdruck = 0; |
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| 1246 | killagreg | 399 | } |
| 1166 | hbuss | 400 | kanal = AD_NICK; |
| 401 | break; |
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| 402 | case 25: |
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| 403 | nick1 += ADC; |
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| 404 | kanal = AD_ROLL; |
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| 405 | break; |
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| 406 | case 26: |
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| 407 | roll1 += ADC; |
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| 408 | kanal = AD_ACC_X; |
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| 409 | break; |
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| 410 | case 27: |
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| 411 | Aktuell_ax = ADC - NeutralAccX; |
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| 412 | accx += Aktuell_ax; |
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| 413 | kanal = AD_GIER; |
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| 414 | break; |
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| 415 | case 28: |
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| 416 | if(PlatinenVersion == 10) AdWertGier = (ADC + gier1 + 2) / 4; |
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| 1246 | killagreg | 417 | else |
| 1166 | hbuss | 418 | if(PlatinenVersion == 20) AdWertGier = 2047 - (ADC + gier1 + 1) / 2; |
| 419 | else AdWertGier = (ADC + gier1 + 1) / 2; |
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| 420 | kanal = AD_NICK; |
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| 421 | break; |
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| 422 | case 29: |
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| 423 | nick1 += ADC; |
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| 424 | kanal = AD_ROLL; |
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| 425 | break; |
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| 426 | case 30: |
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| 427 | roll1 += ADC; |
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| 428 | kanal = AD_ACC_Y; |
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| 429 | break; |
||
| 430 | case 31: |
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| 431 | Aktuell_ay = NeutralAccY - ADC; |
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| 432 | AdWertAccRoll = (Aktuell_ay + accy); |
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| 433 | kanal = AD_NICK; |
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| 434 | break; |
||
| 435 | case 32: |
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| 436 | AdWertNick = (ADC + nick1 + 3) / 5; |
||
| 437 | nick_filter = (long) (1 * (long) nick_filter + 4 * (long)(ADC + nick1) + 1) / 2; |
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| 438 | if(PlatinenVersion == 10) { AdWertNick /= 2;nick_filter /=2;} |
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| 439 | HiResNick = nick_filter - 20 * AdNeutralNick; |
||
| 440 | AdWertNickFilter = (long)(3L * (long)AdWertNickFilter + HiResNick + 2) / 4; |
||
| 1246 | killagreg | 441 | DebugOut.Analog[21] = AdWertNickFilter / 4; |
| 1166 | hbuss | 442 | kanal = AD_ROLL; |
| 443 | break; |
||
| 444 | case 33: |
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| 445 | AdWertRoll = (ADC + roll1 + 3) / 5; |
||
| 446 | roll_filter = (long)(1 * (long)roll_filter + 4 * (long)(ADC + roll1) + 1) / 2; |
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| 447 | if(PlatinenVersion == 10) { AdWertRoll /= 2;roll_filter /=2;} |
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| 448 | HiResRoll = roll_filter - 20 * AdNeutralRoll; |
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| 449 | AdWertRollFilter = (long)(3L * (long)AdWertRollFilter + HiResRoll + 2) / 4; |
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| 450 | DebugOut.Analog[22] = AdWertRollFilter / 4; |
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| 451 | kanal = AD_ACC_X; |
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| 452 | break; |
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| 453 | case 34: |
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| 454 | Aktuell_ax = ADC - NeutralAccX; |
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| 455 | AdWertAccNick = (Aktuell_ax + accx); |
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| 456 | kanal = AD_NICK; |
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| 457 | state = 0; |
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| 458 | AdReady = 1; |
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| 459 | ZaehlMessungen++; |
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| 460 | break; |
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| 1246 | killagreg | 461 | default: |
| 1166 | hbuss | 462 | kanal = 0; |
| 463 | state = 0; |
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| 464 | break; |
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| 1246 | killagreg | 465 | } |
| 1166 | hbuss | 466 | ADMUX = kanal; |
| 467 | if(state != 0) ANALOG_ON; |
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| 468 | } |
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| 1171 | hbuss | 469 | */ |