用质点能量状态近似法来研究飞机综合飞行性能管理技求.首先介绍了飞行性能优化的原理和算法,然后讨论了综合飞行轨迹/速度控制系统——总能量控制系统(TECS),并分析与设计了最优轨迹制导算法,它将性能优化结果直接与总能量控制系统联系在一起,形成综合飞 行性能管理系统.对某型运输机模型的设计与仿真结果证明了该系统所获得的满意性能。 The method of approximation of mass energy states is used to study the performance management of aircraft integrated flight.Firstly, the principle and algorithm of flight performance optimization are introduced, and then the integrated flight path / speed control system-total energy control system (TECS) is discussed. The optimal trajectory guidance algorithm is designed, which integrates the performance optimization results directly with the total energy control system to form an integrated flight performance management system. The design and simulation results of a transport aircraft model demonstrate the satisfactory performance of the system.