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自动着舰纵向飞行控制系统操纵性能优化
引用本文:董然,张鲲鹏,王啸枫,王立鹏,李佳桐.自动着舰纵向飞行控制系统操纵性能优化[J].科技导报(北京),1980,38(21):144-149.
作者姓名:董然  张鲲鹏  王啸枫  王立鹏  李佳桐
作者单位:1. 北京石油化工学院信息工程学院, 北京 102617;
2. 中国船舶工业系统工程研究院航空系统研究所, 北京 100094;
3. 哈尔滨工程大学智能科学与工程学院, 哈尔滨 150001;
4. 中船重工集团公司第704研究所, 上海 200031
基金项目:国家自然科学基金项目(61803116);国防科工局技术基础科研项目(JSZL2017206B005);中央高校基本科研业务费专项资金资助项目(3072019CFJ0405)
摘    要: 自动着舰引导系统能辅助高性能舰载机实现全自动安全、平稳着舰,其飞行控制系统须具备良好操纵性能。基于系统稳定性理论、F/A-18A舰载机测试数据和控制系统时域响应优化方法,提出了一种参数设计方法,“自内向外”逐环优化了自动着舰纵向飞行控制系统参数。仿真验证表明,该系统经参数整定后的指令响应优于F/A-18A的测试结果。

关 键 词:自动着舰    操纵性    纵向控制    飞行数据

Longitudinal maneuverability optimization of flight control in autonomous carrier landing
DONG Ran,ZHANG Kunpeng,WANG Xiaofeng,WANG Lipeng,LI Jiatong.Longitudinal maneuverability optimization of flight control in autonomous carrier landing[J].Science & Technology Review,1980,38(21):144-149.
Authors:DONG Ran  ZHANG Kunpeng  WANG Xiaofeng  WANG Lipeng  LI Jiatong
Institution:1. College of Information Engineering, Beijing Institute of Petrochemical Technology, Beijing 102617, China;
2. Aviation System Research Department, SERI, Beijing 100094, China;
3. College of Intelligent Systems Science and Engineering, Harbin Engineering University, Harbin 150001, China;
4. No. 704 Research Institute, China Shipping Industry Corporation, Shanghai 200031, China
Abstract:Automatic carrier landing system (ACLS) permits high performance carrier-based aircraft to achieve autonomous safe and stable landing, thus its flight control system requires good maneuverability. In this paper, based on system stability theories, test data of F/A-18A fighter aircraft, and the response optimization tools of MATLAB, a novel parameter design method is proposed, and applied to optimizing the parameters of ACLS longitudinal flight control system in a loop by loop and from inside to outside manner. Simulation results show that the system with calibrated parameters has a better performance in responding to the command signal than that of F/A-18A aircraft.
Keywords:
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