Design and evaluation of a post-stall maneuverable flight control law based on nonlinear dynamic inversion

The paper uses nonlinear dynamic inversion combined with flight quality requirements to design flight control laws for a supermaneuverable aircraft, and introduces a new control allocation strategy in combination of aero control surfaces and thrust vectoring based on daisy-chaining algorithm and least-energy method. After Optimizing the configuration and parameters of the control laws, it uses several paragraphs to take robust analyse and Evaluation, with the employing of Bode diagram and Neal-Smith standard. It puts forward the cobra maneuver simulation with a 3D display at last. The simulation results show that the control laws perform excellently not only at the normal flight envelope but also at high angle of attack.