#include "SIM_Airspeed_DLVR.h" #include "SITL.h" int SITL::Airspeed_DLVR::rdwr(I2C::i2c_rdwr_ioctl_data *&data) { struct I2C::i2c_msg &msg = data->msgs[0]; if (msg.flags == I2C_M_RD) { // driver is attempting to receive reading... if (msg.len != 4) { AP_HAL::panic("Unexpected message length (%u)", msg.len); } uint8_t status = 0; if (last_sent_ms == last_update_ms) { status |= 0b10; } last_sent_ms = last_update_ms; // if (electrical_fault_or_bad_config) { // status |= 0b11; // } // calculation of packed-pressure value: // this is TYPE_I2C_DLVR_5IN const uint8_t range_inH2O = 5; #define DLVR_OFFSET 8192.0f #define DLVR_SCALE 16384.0f // const float pressure_pascals = 1555.2f; // maximum transportable const float press_h2o = pressure * (1.0f/INCH_OF_H2O_TO_PASCAL); const uint32_t pressure_raw = ((press_h2o / (1.25f * 2.0f * range_inH2O)) * DLVR_SCALE) + DLVR_OFFSET; // calculation of packed-temperature value const uint32_t temp_raw = (temperature + 50.0f) * (2047.0f/200.0f); const uint32_t packed = (status << 30) | ((pressure_raw & 0x3fff) << 16) | ((temp_raw & 0x7ff) << 5); msg.buf[0] = (packed >> 24) & 0xff; msg.buf[1] = (packed >> 16) & 0xff; msg.buf[2] = (packed >> 8) & 0xff; msg.buf[3] = (packed >> 0) & 0xff; return 0; } AP_HAL::panic("Should never be written to"); } void SITL::Airspeed_DLVR::update(const class Aircraft &aircraft) { const uint32_t now_ms = AP_HAL::millis(); if (now_ms - last_update_ms < 50) { // 20Hz return; } last_update_ms = now_ms; pressure = AP::sitl()->state.airspeed_raw_pressure[0]; float sim_alt = AP::sitl()->state.altitude; sim_alt += 2 * rand_float(); float sigma, delta, theta; AP_Baro::SimpleAtmosphere(sim_alt * 0.001f, sigma, delta, theta); // To Do: Add a sensor board temperature offset parameter temperature = (KELVIN_TO_C(SSL_AIR_TEMPERATURE * theta)) + 25.0; }