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split takeoff into 2 phases, reseting integrators when still on runway
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@@ -1046,7 +1046,7 @@ FixedwingAttitudeControl::task_main()
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}
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float yaw_u = 0.0f;
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if (_att_sp.fw_control_wheel == true) {
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if (_att_sp.fw_control_yaw == true) {
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yaw_u = _wheel_ctrl.control_bodyrate(control_input);
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}
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