mirror of https://github.com/ArduPilot/ardupilot
Copter: use pilot_desired_throttle rather than limit_throttle_out in stabilize and acro.
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f3dc805978
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7d70762053
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@ -28,21 +28,21 @@ void ModeAcro::run()
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motors->set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED);
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}
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bool limit_throttle_out = false;
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float pilot_desired_throttle = get_pilot_desired_throttle();
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switch (motors->get_spool_state()) {
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case AP_Motors::SpoolState::SHUT_DOWN:
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// Motors Stopped
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attitude_control->reset_target_and_rate(true);
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attitude_control->reset_rate_controller_I_terms();
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limit_throttle_out = true;
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pilot_desired_throttle = 0.0f;
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break;
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case AP_Motors::SpoolState::GROUND_IDLE:
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// Landed
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attitude_control->reset_target_and_rate();
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attitude_control->reset_rate_controller_I_terms_smoothly();
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limit_throttle_out = true;
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pilot_desired_throttle = 0.0f;
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break;
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case AP_Motors::SpoolState::THROTTLE_UNLIMITED:
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@ -66,9 +66,7 @@ void ModeAcro::run()
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}
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// output pilot's throttle without angle boost
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attitude_control->set_throttle_out(limit_throttle_out ? 0 : get_pilot_desired_throttle(),
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false,
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copter.g.throttle_filt);
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attitude_control->set_throttle_out(pilot_desired_throttle, false, copter.g.throttle_filt);
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}
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bool ModeAcro::init(bool ignore_checks)
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@ -32,21 +32,21 @@ void ModeStabilize::run()
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motors->set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED);
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}
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bool limit_throttle_out = false;
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float pilot_desired_throttle = get_pilot_desired_throttle();
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switch (motors->get_spool_state()) {
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case AP_Motors::SpoolState::SHUT_DOWN:
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// Motors Stopped
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attitude_control->reset_yaw_target_and_rate();
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attitude_control->reset_rate_controller_I_terms();
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limit_throttle_out = true;
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pilot_desired_throttle = 0.0f;
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break;
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case AP_Motors::SpoolState::GROUND_IDLE:
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// Landed
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attitude_control->reset_yaw_target_and_rate();
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attitude_control->reset_rate_controller_I_terms_smoothly();
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limit_throttle_out = true;
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pilot_desired_throttle = 0.0f;
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break;
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case AP_Motors::SpoolState::THROTTLE_UNLIMITED:
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@ -66,7 +66,5 @@ void ModeStabilize::run()
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attitude_control->input_euler_angle_roll_pitch_euler_rate_yaw(target_roll, target_pitch, target_yaw_rate);
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// output pilot's throttle
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attitude_control->set_throttle_out(limit_throttle_out ? 0 : get_pilot_desired_throttle(),
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true,
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g.throttle_filt);
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attitude_control->set_throttle_out(pilot_desired_throttle, true, g.throttle_filt);
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}
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