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fix MEAS airspeed and airspeed calibration
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@@ -54,8 +54,8 @@
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struct differential_pressure_s {
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uint64_t timestamp; /**< microseconds since system boot, needed to integrate */
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uint64_t error_count;
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uint16_t differential_pressure_pa; /**< Differential pressure reading */
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uint16_t max_differential_pressure_pa; /**< Maximum differential pressure reading */
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float differential_pressure_pa; /**< Differential pressure reading */
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float max_differential_pressure_pa; /**< Maximum differential pressure reading */
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float voltage; /**< Voltage from analog airspeed sensors (voltage divider already compensated) */
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float temperature; /**< Temperature provided by sensor */
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