摘要
讨论了一种具有飞行与推力综合系统的舰载机自动着舰控制系统的设计方法。结合国产某型飞机,首先分析了基于俯仰姿态的升降速率控制系统的结构与控制规律;然后,对飞机进场功率补偿系统的结构与控制规律进行了分析;最后,在同时考虑飞行控制系统与发动机推力补偿控制系统的条件下,对该综合系统的控制规律进行了设计与仿真,并提供了仿真结果。
A design method of the automatic control systems with Integrated flight and thrust controls for landing on carrier is discussed in this paper. The paper first analyzes the longitudinal flight control system and designs the h-Dot control law based on the pitch attitude; then, analyzes the control law of the power compensation system for landing approach;and finally, designs the control laws of the Integrated system. The simulation results are also provided.
出处
《飞行力学》
CSCD
北大核心
1997年第1期56-59,共4页
Flight Dynamics
关键词
飞行控制
推力控制
综合系统
舰载机
Flight control
Thrust control
Integrated system
Aircraft on carrier
Automatic landing on carrier