TradHeli: remove calls to get_manual_collective in auto throttle
set_collective_for_landing method makes this unnecessary
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@ -2004,13 +2004,8 @@ void update_throttle_mode(void)
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get_throttle_althold_with_slew(wp_nav.get_desired_alt(), -wp_nav.get_descent_velocity(), wp_nav.get_climb_velocity());
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set_target_alt_for_reporting(wp_nav.get_desired_alt()); // To-Do: return get_destination_alt if we are flying to a waypoint
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}else{
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#if FRAME_CONFIG == HELI_FRAME
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// collective pitch should not be full negative to avoid harshing the mechanics. Use Stab Coll Min.
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set_throttle_out(motors.get_manual_collective_min(), false);
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#else
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// pilot's throttle must be at zero so keep motors off
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set_throttle_out(0, false);
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#endif // HELI_FRAME
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// deactivate accel based throttle controller
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throttle_accel_deactivate();
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set_target_alt_for_reporting(0);
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@ -917,17 +917,7 @@ get_throttle_accel(int16_t z_target_accel)
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d = g.pid_throttle_accel.get_d(z_accel_error, .01f);
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#if FRAME_CONFIG == HELI_FRAME
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if (ap.takeoff_complete == true){
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output = constrain_float(p+i+d+g.throttle_cruise, g.throttle_min, g.throttle_max);
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} else {
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// Avoid harshing the mechanics pushing into the ground
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// stab_col_min should gently push down on the ground
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output = constrain_float(p+i+d+g.throttle_cruise, motors.get_manual_collective_min(), motors.get_manual_collective_max());
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}
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#else
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output = constrain_float(p+i+d+g.throttle_cruise, g.throttle_min, g.throttle_max);
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#endif // HELI_FRAME
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#if LOGGING_ENABLED == ENABLED
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// log output if PID loggins is on and we are tuning the yaw
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