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碟形飞行器复合控制的非线性分配策略研究
引用本文:徐胜红,盛忠培,顾文锦.碟形飞行器复合控制的非线性分配策略研究[J].弹箭与制导学报,2006,26(1):8-11.
作者姓名:徐胜红  盛忠培  顾文锦
作者单位:1. 海军航空工程学院,山东,烟台,264001
2. 海装军械保障部,北京,100841
基金项目:总装预研重点基金项目(编号:6140511)
摘    要:针对碟形飞行器变质量矩/推力矢量复合控制系统,研究了以输出误差为参考量的非线性控制分配策略。仿真表明,这一设计实现了两种控制方式的优势互补.又避免了强制切换控制方式所引起的控制扰动,达到了良好的控制性能。

关 键 词:碟形飞行器  复合控制  分配策略
收稿时间:2005-06-22
修稿时间:2005-06-22

Nonlinear Distribution Strategy for Compound Control Over Flying Saucer
XU Shenghong,SHENG Zhongpei,GU Wenjin.Nonlinear Distribution Strategy for Compound Control Over Flying Saucer[J].Journal of Projectiles Rockets Missiles and Guidance,2006,26(1):8-11.
Authors:XU Shenghong  SHENG Zhongpei  GU Wenjin
Affiliation:1. Naval Aeronautical Engineering Institute,Shandong Yantai 264001 ,China; 2, Ordnance Support Branch of NED,Beijing 100841 ,China
Abstract:Nonlinear distribution strategy is proposed for moving-mass/thrust-vectoring compound control over flying saucer based on output error. Simulation shows that with the design the two control units complement each other avoiding control disturbance produced by control switch, and obtains preferable control results.
Keywords:flying saucer  compound control  distribution strategy
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