海军航空工程学院学报2011，Vol.26Issue(3)：241-245,5.
某型飞机角位移自动驾驶仪比例式控制规律设计与仿真
Design and Simulation of the Proportional Control Law for Aircraft Angular Displacement Autopilot
摘要
Abstract
In modern aircraft flight, more and more complex aircraft mission performance requirements had become more sophisticated, angular displacement autopilot control law design to ensure the merits of the aircraft flying normally plays an important role. For this reason, a certain type of aircraft autopilot control law of the proportion of type design, simulation analysis of the rate feedback and the principle of selecting and then a good performance of the proportional autopilot control law. Comparison by a large number of simulation and verification were that the designed autopilot proportional control law in good control system had good dynamic and static performance and the system's time domain and frequency domain indices could meet the system requirements.关键词
比例式控制规律/舵回路/俯仰角速率反馈/系统阻尼/仿真Key words
proportional control law/ rudder loop/ pitch angle rate feedback/ system damping/ simulation引用本文复制引用
程继红,曲东才,卢斌文,于德海..某型飞机角位移自动驾驶仪比例式控制规律设计与仿真[J].海军航空工程学院学报,2011,26(3):241-245,5.基金项目
国家自然科学基金资助项目(60774016) （60774016）
