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https://github.com/PX4/PX4-Autopilot.git
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vtol attitude control: fixed code style
Signed-off-by: tumbili <roman@px4.io>
This commit is contained in:
@@ -188,7 +188,7 @@ void Standard::update_vtol_state()
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} else if (_vtol_schedule.flight_mode == TRANSITION_TO_FW) {
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// continue the transition to fw mode while monitoring airspeed for a final switch to fw mode
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if (((_params_standard.airspeed_mode == control_state_s::AIRSPD_MODE_DISABLED ||
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_airspeed->indicated_airspeed_m_s >= _params_standard.airspeed_trans) &&
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_airspeed->indicated_airspeed_m_s >= _params_standard.airspeed_trans) &&
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(float)hrt_elapsed_time(&_vtol_schedule.transition_start)
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> (_params_standard.front_trans_time_min * 1000000.0f)) ||
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can_transition_on_ground()) {
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@@ -250,11 +250,13 @@ void Standard::update_transition_state()
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_mc_yaw_weight = weight;
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_mc_throttle_weight = weight;
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// time based blending when no airspeed sensor is set
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// time based blending when no airspeed sensor is set
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} else if (_params_standard.airspeed_mode == control_state_s::AIRSPD_MODE_DISABLED &&
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(float)hrt_elapsed_time(&_vtol_schedule.transition_start) < (_params_standard.front_trans_time_min * 1000000.0f)
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) {
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float weight = 1.0f - (float)(hrt_elapsed_time(&_vtol_schedule.transition_start) / (_params_standard.front_trans_time_min * 1000000.0f));
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(float)hrt_elapsed_time(&_vtol_schedule.transition_start) < (_params_standard.front_trans_time_min * 1000000.0f)
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) {
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float weight = 1.0f - (float)(hrt_elapsed_time(&_vtol_schedule.transition_start) /
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(_params_standard.front_trans_time_min * 1000000.0f));
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_mc_roll_weight = weight;
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_mc_pitch_weight = weight;
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_mc_yaw_weight = weight;
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