| 102,24 → 102,24 |
|---|
| "M2 ", |
| "M3 ", |
| "M4 ", |
| "pdpart ", |
| "control ", //15 |
| "controlActivity ", |
| "accVector ", //15 |
| "RC Stick P ", |
| "RC Stick R ", |
| "Stick P w GPS ", |
| "Stick R w GPS ", |
| "RC Stick T ", |
| "RC Stick Y ", |
| "Stick P w Emerg.", //20 |
| "Stick R w Emerg.", |
| "Height[dm] ", |
| "dHeight ", |
| "Altitude ", |
| " ", //25 |
| "Altitude ", |
| "EFT ", //25 |
| "naviPitch ", |
| "naviRoll ", |
| "i part contrib ", |
| "HeadingError ", |
| "Magnetic Heading", //30 |
| "GPS Datasets " |
| " ", |
| " ", //30 |
| " " |
| }; |
| |
| /****************************************************************/ |
| 200,10 → 200,6 |
|---|
| versionInfo.protoMajor = VERSION_SERIAL_MAJOR; |
| versionInfo.protoMinor = VERSION_SERIAL_MINOR; |
| |
| for (uint8_t i=0; i<32; i++) { |
| debugOut.analog[i] = i; |
| } |
| |
| // restore global interrupt flags |
| SREG = sreg; |
| } |
| 290,8 → 286,8 |
|---|
| tmpchecksum += txd_buffer[i]; |
| } |
| tmpchecksum %= 4096; |
| txd_buffer[i++] = '=' + tmpchecksum >> 6; |
| txd_buffer[i++] = '=' + tmpchecksum & 0x3F; |
| txd_buffer[i++] = '=' + (tmpchecksum >> 6); |
| txd_buffer[i++] = '=' + (tmpchecksum & 0x3F); |
| txd_buffer[i++] = '\r'; |
| txd_complete = FALSE; |
| UDR0 = txd_buffer[0]; // initiates the transmittion (continued in the TXD ISR) |
| 514,7 → 510,11 |
|---|
| else if (pRxData[0] > 5) |
| pRxData[0] = 5; // limit to 5 |
| // load requested parameter set |
| |
| debugOut.analog[30] = staticParams.GPSMininumSatellites; |
| |
| paramSet_readFromEEProm(pRxData[0]); |
| |
| tempchar[0] = pRxData[0]; |
| tempchar[1] = EEPARAM_REVISION; |
| tempchar[2] = sizeof(staticParams); |
| 530,6 → 530,8 |
|---|
| { |
| memcpy(&staticParams, (uint8_t*) &pRxData[3], sizeof(staticParams)); |
| paramSet_writeToEEProm(pRxData[0]); |
| setActiveParamSet(pRxData[0]); |
| configuration_paramSetDidChange(); |
| tempchar[0] = getActiveParamSet(); |
| beepNumber(tempchar[0]); |
| } else { |