#include "SIM_MS5611.h" #include #include using namespace SITL; // forward conversion, copied from driver: void MS5611::convert_forward(int32_t D1, int32_t D2, float &P_Pa, float &Temp_C) { float dT; float TEMP; float OFF; float SENS; dT = D2-(((uint32_t)prom[5])<<8); TEMP = (dT * prom[6])/8388608; OFF = prom[2] * 65536.0f + (prom[4] * dT) / 128; SENS = prom[1] * 32768.0f + (prom[3] * dT) / 256; TEMP += 2000; if (TEMP < 2000) { // second order temperature compensation when under 20 degrees C float T2 = (dT*dT) / 0x80000000; float Aux = sq(TEMP-2000.0); float OFF2 = 2.5f*Aux; float SENS2 = 1.25f*Aux; if (TEMP < -1500) { // extra compensation for temperatures below -15C OFF2 += 7 * sq(TEMP+1500); SENS2 += sq(TEMP+1500) * 11.0*0.5; } TEMP = TEMP - T2; OFF = OFF - OFF2; SENS = SENS - SENS2; } P_Pa = (D1*SENS/2097152 - OFF)/32768; Temp_C = TEMP * 0.01f; } void MS5611::convert(float P_Pa, float Temp_C, uint32_t &D1, uint32_t &D2) { int64_t TEMP = Temp_C * 100.0f; const float dT = (TEMP-2000.0) / (prom[6]/8388608.0); float OFF = prom[2] * 65536.0f + (prom[4] * dT) / 128; float SENS = prom[1] * 32768.0f + (prom[3] * dT) / 256; if (TEMP < 2000) { // second order temperature compensation when under 20 degrees C float T2 = (dT*dT) / 0x80000000; float Aux = sq(TEMP-2000.0); float OFF2 = 2.5f*Aux; float SENS2 = 1.25f*Aux; if (TEMP < -1500) { // extra compensation for temperatures below -15C OFF2 += 7 * sq(TEMP+1500); SENS2 += sq(TEMP+1500) * 11.0*0.5; } TEMP = TEMP - T2; OFF = OFF - OFF2; SENS = SENS - SENS2; } D1 = ((P_Pa*32768.0)+OFF) / (SENS/2097152.0); D2 = dT + (((uint32_t)prom[5])<<8); float f_P_Pa; float f_Temp_C; convert_forward(D1, D2, f_P_Pa, f_Temp_C); if (fabs(f_P_Pa - P_Pa) > 1) { AP_HAL::panic("Invalid pressure conversion"); } if (fabs(f_Temp_C - Temp_C) > 0.1) { AP_HAL::panic("Invalid temperature conversion"); } } void MS5611::get_pressure_temperature_readings(float &P_Pa, float &Temp_C) { float sigma, delta, theta; float sim_alt = AP::sitl()->state.altitude; sim_alt += 2 * rand_float(); AP_Baro::SimpleAtmosphere(sim_alt * 0.001f, sigma, delta, theta); P_Pa = SSL_AIR_PRESSURE * delta; Temp_C = (30.0 + C_TO_KELVIN) * theta - C_TO_KELVIN; // Assume 30 degrees at sea level - converted to degrees Kelvin }