forked from Archive/PX4-Autopilot
compute atmospheric pressure from altitude
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@ -43,6 +43,10 @@ using namespace simulator;
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#define UDP_PORT 14550
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#define UDP_PORT 14550
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#define PIXHAWK_DEVICE "/dev/ttyACM0"
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#define PIXHAWK_DEVICE "/dev/ttyACM0"
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#define PRESS_GROUND 101325.0f
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#define DENSITY 1.2041f
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#define GRAVITY 9.81f
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static const uint8_t mavlink_message_lengths[256] = MAVLINK_MESSAGE_LENGTHS;
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static const uint8_t mavlink_message_lengths[256] = MAVLINK_MESSAGE_LENGTHS;
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static const uint8_t mavlink_message_crcs[256] = MAVLINK_MESSAGE_CRCS;
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static const uint8_t mavlink_message_crcs[256] = MAVLINK_MESSAGE_CRCS;
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@ -183,7 +187,8 @@ void Simulator::update_sensors(struct sensor_combined_s *sensor, mavlink_hil_sen
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write_mag_data((void *)&mag);
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write_mag_data((void *)&mag);
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RawBaroData baro;
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RawBaroData baro;
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baro.pressure = imu->abs_pressure;
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// calculate air pressure from altitude (valid for low altitude)
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baro.pressure = PRESS_GROUND - GRAVITY * DENSITY * imu->pressure_alt;
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baro.altitude = imu->pressure_alt;
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baro.altitude = imu->pressure_alt;
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baro.temperature = imu->temperature;
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baro.temperature = imu->temperature;
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