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空间目标姿态吊挂控制装置半实物仿真研究
引用本文:郑宾,郑浩鑫,侯文,刘治德,谭文.空间目标姿态吊挂控制装置半实物仿真研究[J].弹箭与制导学报,2006,26(2):45-46,53.
作者姓名:郑宾  郑浩鑫  侯文  刘治德  谭文
作者单位:中北大学仪器科学与动态测试教育部重点实验室,太原,030051
摘    要:文中运用静力学中的空间任意力系平衡的两个必要与充分条件,结合实际目标姿态吊挂控制系统的结构特性,建立了空间目标吊挂模型姿态调整的数学模型,后联立并求解多元方程组,得到在各种确定姿态下的各吊绳的长度,准确的实现整个目标姿态吊挂控制系统对目标模型的姿态调整.

关 键 词:目标模型  平衡力系  吊挂目标控制  姿态调整
收稿时间:2005-01-13
修稿时间:2005-01-13

Hardware in the Loop Simulating for Space Target Attiude Suspending Device
ZHENG Bin,ZHENG Hao-xin,HOU Wen,LIU Zhi-de,TAN Wen.Hardware in the Loop Simulating for Space Target Attiude Suspending Device[J].Journal of Projectiles Rockets Missiles and Guidance,2006,26(2):45-46,53.
Authors:ZHENG Bin  ZHENG Hao-xin  HOU Wen  LIU Zhi-de  TAN Wen
Abstract:This paper is based on the necessary condition and sufficient condition for the balance of any space force system in static mechanics, in combination with the structural properties of the actual target attitude suspending control system, the mathematical model for attitude adjustment of the space target suspending device is created subtly. By combining and solving the multl-equation, the length of the suspending rope under various attitude condition are obtained, finally to realize the attitude adjustment of the targeted model by the control system.
Keywords:target model  balance mechanics  suspending target control l attitude adjustment
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