On optimal guidance arithmetic of Super-maneuverable aircraft

Due to the complexity of maneuverability, Super-maneuver attack guidance of modern aircraft has become the most important function to be immediately solved and perfectly completed. Proceed from the maneuvering optimization position and based on the optimal control theory,the optimal angle maneuver guidance arithmatic is proposed. On the basis of aircraft maneuver guidance algorithm, we come up with a variety of constraint condition, optimized index and optimization rule and present a set of steepest optimal angle maneuver guidance algorithm, and the validity and feasibility of the steepest optimal angle maneuver guidance algorithm has been comfirmed by the super-maneuver guidance simulation.