摘要：AbstractIn this paper a control topology with limited pitch and roll authority is described for automatic leveling of a fighter aircraft from disorientation. The proposed scheme provides recovery capability for an aircraft from any bank angle within the envelope defined by airspeed (CAS), angle of attack (AoA) and flight path angle to steady level flight. The control algorithm generates pitch and roll commands to bring the aircraft to level flight without violating the specified aircraft parameter limits. The command generation scheme is validated through nonlinear simulation and flight tested on a fighter aircraft for different flight conditions and the results are presented.
