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无人动力伞建模及预测控制
引用本文:谢志刚,陈自力,刘雨田. 无人动力伞建模及预测控制[J]. 军械工程学院学报, 2011, 0(2): 52-55
作者姓名:谢志刚  陈自力  刘雨田
作者单位:军械工程学院光学与电子工程系;机械化步兵学院教研部;
摘    要:建立了无人动力伞6自由度控制模型,依托该模型分析了系统的动力学特性与动态性能,阐述了基于预测控制算法的无人动力伞系统飞行控制律,并在实际飞行条件下,验证飞行控制系统的控制精度。

关 键 词:无人动力伞系统  预测控制  建模

Modeling and Predictive Control for Unmanned Powered Parafoil
XIE Zhi-gang,CHEN Zi-li,LIU Yu-tian. Modeling and Predictive Control for Unmanned Powered Parafoil[J]. Journal of Ordnance Engineering College, 2011, 0(2): 52-55
Authors:XIE Zhi-gang  CHEN Zi-li  LIU Yu-tian
Affiliation:XIE Zhi-gang1,CHEN Zi-li1,LIU Yu-tian2(1.Department of Optics and Electronics Engineering,Ordnance Engineering College,Shijiazhuang 050003,China,2.Department of Teaching and Research,Mechanized Infantry Academy,Shijiazhuang 050083,China)
Abstract:The paper develops a six degree-of-freedom model of unmanned powered parafoil to analyze the dynamics and kinematics of the parafoil system.Model predictive control is proposed as a control strategy,which is suitable for optimizing the performance of powered parafoil.The feasibility and control accuracy of the control law are verified in the flying experiment.
Keywords:unmanned powered parafoil  predictive control  modeling  
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