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考察了求解输入类飞行逆动力学问题的微分迭代与积分迭代算法；探讨了利用逆动力学确定过失速机动操纵效能要求问题，这构成了进一步提出过失速机动飞机设计简化判据的数值基础；利用逆动力学设计机动发生模块进行飞控系统的最外环控制，以便跟踪期望的复杂机动轨迹．飞机最速反向示例及其它数值仿真结果表明设计思想与算法是可行的．
The differential-iterative and integral-iterative algorithms for the inverse kinematics of input flight are investigated. The application of inverse dynamics to determine the maneuvering performance requirements for stalling maneuvers is discussed. This results in a further numerical solution to the simplified design criteria of the stalling maneuvering aircraft Based on the inverse kinematics, a maneuvering module is designed to control the outermost loop of the flight control system to track the desired complex maneuvering trajectory. The airplane reverse speed example and other numerical simulation results show that the design idea and algorithm are feasible.