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vtol_type: remove unused variable and function for deceleration pitch integral (#24419)

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This functionality was moved to FlightTaskTransition and the variable was forgotten in 079b756f1b
This commit is contained in:
Matthias Grob
2025-02-26 12:37:21 +00:00
committed by GitHub
parent 5d2814f6c9
commit f69361f742
2 changed files with 0 additions and 6 deletions
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3
src/modules/vtol_att_control/vtol_type.cpp
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@@ -100,8 +100,6 @@ void VtolType::parameters_update()
void VtolType::update_mc_state()
{
resetAccelToPitchPitchIntegrator();
// copy virtual attitude setpoint to real attitude setpoint
memcpy(_v_att_sp, _mc_virtual_att_sp, sizeof(vehicle_attitude_setpoint_s));
@@ -113,7 +111,6 @@ void VtolType::update_mc_state()
void VtolType::update_fw_state()
{
resetAccelToPitchPitchIntegrator();
_last_thr_in_fw_mode = _vehicle_thrust_setpoint_virtual_fw->xyz[0];
// copy virtual attitude setpoint to real attitude setpoint

3
src/modules/vtol_att_control/vtol_type.h
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@@ -313,8 +313,6 @@ protected:
float _quadchute_ref_alt{NAN}; // altitude (AMSL) reference to compute quad-chute altitude loss condition
float _accel_to_pitch_integ = 0;
bool _quadchute_command_treated{false};
bool isFrontTransitionCompleted();
@@ -364,7 +362,6 @@ protected:
private:
hrt_abstime _throttle_blend_start_ts{0}; // time at which we start blending between transition throttle and fixed wing throttle
void resetAccelToPitchPitchIntegrator() { _accel_to_pitch_integ = 0.f; }
bool shouldBlendThrottleAfterFrontTransition() { return _throttle_blend_start_ts != 0; };
void stopBlendingThrottleAfterFrontTransition() { _throttle_blend_start_ts = 0; }