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| 飞机γ角姿态控制系统方案设计及仿真 | |
| 引用本文： | 张卓,曲东才,陈勇,郭强.飞机γ角姿态控制系统方案设计及仿真[J].海军航空工程学院学报,2012,27(4):451-455. |
| 作者姓名： | 张卓 曲东才 陈勇 郭强 |
| 作者单位： | 1. 海军装备部飞机办,北京 100841 2. 海军航空工程学院控制工程系,山东 烟台 264001 3. 海军装备部西安军事代表局,西安 710054 |
| 基金项目： | 国家自然科学基金资助项目（60774016） |
| 摘 要： | 在简要分析飞机侧向控制系统运动模态基础上,对飞机γ角姿态控制系统结构方案进行设计并进行仿真验证。仿真结果显示,所设计的飞机γ角姿态控制系统结构方案及其控制规律具有良好抗干扰能力,是合理有效的,从而提出对飞行状态变化剧烈的飞机,应采用控制规律调参措施。 |
| 关 键 词： | 侧向运动模态 γ角姿态控制系统 控制规律传动比 调参 |
Design and Simulation ofAero γAngle Attitude Control System |
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| ZHANG Zhuo,QU Dong-cai,CHEN Yong and GUO Qiang.Design and Simulation ofAero γAngle Attitude Control System[J].Journal of Naval Aeronautical Engineering Institute,2012,27(4):451-455. | |
| Authors: | ZHANG Zhuo QU Dong-cai CHEN Yong and GUO Qiang |
| Institution: | 3 ( 1. Aircraft Office of NED, Beijing 100841, China; 2. Department of Control Engineering, NAAU, Yantai Shandong 264001, China 3. Military Representatives Bureau of NED in Xian Area, Xian 710054, China) |
| Abstract: | On the basis of synopsis analysis airplane the sport molds of the lateral side control system, the structure control project of aero angle attitude control system was designed and verified by simulation was done. Simulation results show that designed aero angle attitude control system structure project and it＇s control law had good anti-interference ability, and were feasible. Lastly, it was put forward the control law should adopt adjusting parameters measures with flying state violent variety airplane. |
| Keywords: | lateral side sport mold angle attitude control system transmission ratio of control law adjusting parameters simulation |
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