摘要
主要研究舰载飞机在进场下滑着舰过程中的飞行动力学问题。着重讨论了舰载飞机在进场下滑过程中的轨迹保持及其纵向控制,同时给出了此时飞机的飞行自动控制系统和进场功率补偿器系统反馈控制参数的计算方法。
The flight dynamics problems in the process of aircraft approach glide—down and landing are studied. The problems of the approach glide—down path holding and longitudinal control are particularly discussed. At the same time, the ways to calculate the feedback control loop parameters for automatic flight control system and approach power compensator system are given.
出处
《飞行力学》
CSCD
北大核心
1993年第3期31-41,共11页
Flight Dynamics
关键词
舰载飞机
飞行控制
着舰
Shipboard aircraft Flight control Deck landing
