Sub: Clarify that the target_yaw_rate variable is set
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@ -16,7 +16,6 @@ void Sub::stabilize_run()
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{
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uint32_t tnow = AP_HAL::millis();
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float target_roll, target_pitch;
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float target_yaw_rate;
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// if not armed set throttle to zero and exit immediately
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if (!motors.armed()) {
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@ -34,7 +33,7 @@ void Sub::stabilize_run()
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get_pilot_desired_lean_angles(channel_roll->get_control_in(), channel_pitch->get_control_in(), target_roll, target_pitch, aparm.angle_max);
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// get pilot's desired yaw rate
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target_yaw_rate = get_pilot_desired_yaw_rate(channel_yaw->get_control_in());
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float target_yaw_rate = get_pilot_desired_yaw_rate(channel_yaw->get_control_in());
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// call attitude controller
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// update attitude controller targets
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@ -21,7 +21,6 @@ bool Sub::surface_init()
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void Sub::surface_run()
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{
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float target_roll, target_pitch;
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float target_yaw_rate;
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// if not armed set throttle to zero and exit immediately
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if (!motors.armed()) {
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@ -43,7 +42,7 @@ void Sub::surface_run()
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get_pilot_desired_lean_angles(channel_roll->get_control_in(), channel_pitch->get_control_in(), target_roll, target_pitch, aparm.angle_max);
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// get pilot's desired yaw rate
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target_yaw_rate = get_pilot_desired_yaw_rate(channel_yaw->get_control_in());
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float target_yaw_rate = get_pilot_desired_yaw_rate(channel_yaw->get_control_in());
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// call attitude controller
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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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