AP_InertialNav: use references to AHRS and baro
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@ -50,7 +50,7 @@ void AP_InertialNav::update(float dt)
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// check if new gps readings have arrived and use them to correct position estimates
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check_gps();
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Vector3f accel_ef = _ahrs->get_accel_ef();
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Vector3f accel_ef = _ahrs.get_accel_ef();
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// remove influence of gravity
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accel_ef.z += GRAVITY_MSS;
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@ -310,15 +310,12 @@ void AP_InertialNav::check_baro()
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{
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uint32_t baro_update_time;
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if( _baro == NULL )
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return;
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// calculate time since last baro reading (in ms)
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baro_update_time = _baro->get_last_update();
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baro_update_time = _baro.get_last_update();
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if( baro_update_time != _baro_last_update ) {
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const float dt = (float)(baro_update_time - _baro_last_update) * 0.001f; // in seconds
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// call correction method
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correct_with_baro(_baro->get_altitude()*100, dt);
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correct_with_baro(_baro.get_altitude()*100, dt);
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_baro_last_update = baro_update_time;
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}
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}
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@ -34,7 +34,7 @@ class AP_InertialNav
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public:
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// Constructor
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AP_InertialNav( const AP_AHRS* ahrs, AP_Baro* baro, GPS*& gps, GPS_Glitch& gps_glitch ) :
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AP_InertialNav( const AP_AHRS &ahrs, AP_Baro &baro, GPS*& gps, GPS_Glitch& gps_glitch ) :
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_ahrs(ahrs),
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_baro(baro),
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_gps(gps),
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@ -280,8 +280,8 @@ protected:
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uint8_t ignore_error : 3; // the number of iterations for which we should ignore errors
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} _flags;
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const AP_AHRS* const _ahrs; // pointer to ahrs object
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AP_Baro* _baro; // pointer to barometer
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const AP_AHRS &_ahrs; // reference to ahrs object
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AP_Baro &_baro; // reference to barometer
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GPS*& _gps; // pointer to gps
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// XY Axis specific variables
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