/* output MSP protocol from AP_Periph for ArduPilot and INAV Thanks to input from Konstantin Sharlaimov */ #include #include "AP_Periph.h" #ifdef HAL_PERIPH_ENABLE_MSP void AP_Periph_FW::msp_init(AP_HAL::UARTDriver *_uart) { if (_uart) { msp.port.uart = _uart; msp.port.msp_version = MSP::MSP_V2_NATIVE; _uart->begin(115200, 512, 512); } } /* send a MSP packet */ void AP_Periph_FW::send_msp_packet(uint16_t cmd, void *p, uint16_t size) { uint8_t out_buf[size+16] {}; MSP::msp_packet_t pkt = { .buf = { .ptr = out_buf, .end = MSP_ARRAYEND(out_buf), }, .cmd = (int16_t)cmd, .flags = 0, .result = 0, }; sbuf_write_data(&pkt.buf, p, size); sbuf_switch_to_reader(&pkt.buf, &out_buf[0]); MSP::msp_serial_encode(&msp.port, &pkt, MSP::MSP_V2_NATIVE, true); } /* update MSP sensors */ void AP_Periph_FW::msp_sensor_update(void) { if (msp.port.uart == nullptr) { return; } #ifdef HAL_PERIPH_ENABLE_GPS send_msp_GPS(); #endif #ifdef HAL_PERIPH_ENABLE_BARO send_msp_baro(); #endif #ifdef HAL_PERIPH_ENABLE_MAG send_msp_compass(); #endif #ifdef HAL_PERIPH_ENABLE_AIRSPEED send_msp_airspeed(); #endif } #ifdef HAL_PERIPH_ENABLE_GPS /* send MSP GPS packet */ void AP_Periph_FW::send_msp_GPS(void) { MSP::msp_gps_data_message_t p; if (gps.get_type(0) == AP_GPS::GPS_Type::GPS_TYPE_NONE) { return; } if (msp.last_gps_ms == gps.last_message_time_ms(0)) { return; } msp.last_gps_ms = gps.last_message_time_ms(0); const Location &loc = gps.location(0); const Vector3f &vel = gps.velocity(0); p.instance = 0; p.gps_week = gps.time_week(0); p.ms_tow = gps.get_itow(0); p.fix_type = uint8_t(gps.status(0)); p.satellites_in_view = gps.num_sats(0); float hacc=0, vacc=0, sacc=0; gps.horizontal_accuracy(0, hacc); gps.vertical_accuracy(0, vacc); gps.speed_accuracy(0, sacc); p.horizontal_vel_accuracy = sacc*100; p.horizontal_pos_accuracy = hacc*100; p.vertical_pos_accuracy = vacc*100; p.hdop = gps.get_hdop(0); p.longitude = loc.lng; p.latitude = loc.lat; p.msl_altitude = loc.alt; p.ned_vel_north = vel.x*100; p.ned_vel_east = vel.y*100; p.ned_vel_down = vel.z*100; p.ground_course = wrap_360_cd(gps.ground_course(0)*100); float yaw_deg=0, acc; uint32_t time_ms; if (gps.gps_yaw_deg(0, yaw_deg, acc, time_ms)) { p.true_yaw = wrap_360_cd(yaw_deg*100); } else { p.true_yaw = 65535; // unknown } uint64_t tepoch_us = gps.time_epoch_usec(0); time_t utc_sec = tepoch_us / (1000U * 1000U); struct tm tvd {}; struct tm* tm = gmtime_r(&utc_sec, &tvd); p.year = tm->tm_year+1900; p.month = tm->tm_mon; p.day = tm->tm_mday; p.hour = tm->tm_hour; p.min = tm->tm_min; p.sec = tm->tm_sec; send_msp_packet(MSP2_SENSOR_GPS, &p, sizeof(p)); } #endif // HAL_PERIPH_ENABLE_GPS #ifdef HAL_PERIPH_ENABLE_BARO /* send MSP baro packet */ void AP_Periph_FW::send_msp_baro(void) { MSP::msp_baro_data_message_t p; if (msp.last_baro_ms == baro.get_last_update(0)) { return; } if (!baro.healthy()) { // don't send any data return; } msp.last_baro_ms = baro.get_last_update(0); p.instance = 0; p.time_ms = msp.last_baro_ms; p.pressure_pa = baro.get_pressure(); p.temp = baro.get_temperature() * 100; send_msp_packet(MSP2_SENSOR_BAROMETER, &p, sizeof(p)); } #endif // HAL_PERIPH_ENABLE_BARO #ifdef HAL_PERIPH_ENABLE_MAG /* send MSP compass packet */ void AP_Periph_FW::send_msp_compass(void) { MSP::msp_compass_data_message_t p; if (msp.last_mag_ms == compass.last_update_ms(0)) { return; } if (!compass.healthy()) { return; } msp.last_mag_ms = compass.last_update_ms(0); const Vector3f &field = compass.get_field(0); p.instance = 0; p.time_ms = msp.last_mag_ms; p.magX = field.x; p.magY = field.y; p.magZ = field.z; send_msp_packet(MSP2_SENSOR_COMPASS, &p, sizeof(p)); } #endif // HAL_PERIPH_ENABLE_MAG #ifdef HAL_PERIPH_ENABLE_AIRSPEED /* send MSP airspeed packet */ void AP_Periph_FW::send_msp_airspeed(void) { MSP::msp_airspeed_data_message_t p; const uint32_t last_update_ms = airspeed.last_update_ms(); if (msp.last_airspeed_ms == last_update_ms) { return; } if (!airspeed.healthy()) { // we don't report at all for an unhealthy sensor. This maps // to unhealthy in the flight controller driver return; } msp.last_airspeed_ms = last_update_ms; p.instance = 0; p.time_ms = msp.last_airspeed_ms; p.pressure = airspeed.get_corrected_pressure(); float temp; if (!airspeed.get_temperature(temp)) { p.temp = INT16_MIN; //invalid temperature } else { p.temp = temp * 100; } send_msp_packet(MSP2_SENSOR_AIRSPEED, &p, sizeof(p)); } #endif // HAL_PERIPH_ENABLE_AIRSPEED #endif // HAL_PERIPH_ENABLE_MSP