mirror of https://github.com/ArduPilot/ardupilot
AC_AttitudeControl: rate_controller_run_dt() takes dt as last argument
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@ -245,7 +245,7 @@ public:
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virtual void rate_controller_target_reset() {}
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// optional variant to allow running with different dt
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virtual void rate_controller_run_dt(float dt, const Vector3f& gyro) { AP_BoardConfig::config_error("rate_controller_run_dt() must be defined"); };
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virtual void rate_controller_run_dt(const Vector3f& gyro, float dt) { AP_BoardConfig::config_error("rate_controller_run_dt() must be defined"); };
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// Convert a 321-intrinsic euler angle derivative to an angular velocity vector
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void euler_rate_to_ang_vel(const Quaternion& att, const Vector3f& euler_rate_rads, Vector3f& ang_vel_rads);
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@ -439,7 +439,7 @@ void AC_AttitudeControl_Multi::update_throttle_rpy_mix()
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_throttle_rpy_mix = constrain_float(_throttle_rpy_mix, 0.1f, AC_ATTITUDE_CONTROL_MAX);
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}
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void AC_AttitudeControl_Multi::rate_controller_run_dt(float dt, const Vector3f& gyro)
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void AC_AttitudeControl_Multi::rate_controller_run_dt(const Vector3f& gyro, float dt)
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{
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// take a copy of the target so that it can't be changed from under us.
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Vector3f ang_vel_body = _ang_vel_body;
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@ -481,7 +481,7 @@ void AC_AttitudeControl_Multi::rate_controller_target_reset()
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void AC_AttitudeControl_Multi::rate_controller_run()
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{
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Vector3f gyro_latest = _ahrs.get_gyro_latest();
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rate_controller_run_dt(_dt, gyro_latest);
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rate_controller_run_dt(gyro_latest, _dt);
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}
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// sanity check parameters. should be called once before takeoff
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@ -76,7 +76,7 @@ public:
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bool is_throttle_mix_min() const override { return (_throttle_rpy_mix < 1.25f * _thr_mix_min); }
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// run lowest level body-frame rate controller and send outputs to the motors
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void rate_controller_run_dt(float dt, const Vector3f& gyro) override;
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void rate_controller_run_dt(const Vector3f& gyro, float dt) override;
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void rate_controller_target_reset() override;
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void rate_controller_run() override;
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