Application of inverse flight dynamics

The computational technique for inverse flight dynamics, named the derivation-iteration and integration-iteration algorithm, were investigated. The application of inverse dynamics to determine control power requirements for post-stall maneuvering was studied, which may use as the numerical fundamental for simplifying design criteria of the post-stall aircraft. The flight control mode for the outer loop control of the system, named maneuver generator, was designed to track designed complex maneuvering flight trajectory. The simulation results for the rapid heading-reversal maneuver has shown that the design idea and the algorithm are feasible.