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空间目标姿态吊挂控制装置半实物仿真研究

Hardware in the Loop Simulating for Space Target Attiude Suspending Device
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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。 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.
出处 《弹箭与制导学报》 CSCD 北大核心 2006年第2期45-46,53,共3页 Journal of Projectiles,Rockets,Missiles and Guidance
关键词 目标模型 平衡力系 吊挂目标控制 姿态调整 target model balance mechanics suspending target control l attitude adjustment
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参考文献3

  • 1[美]费迪南德P.比尔(Ferdinand P.Beer),E.罗素.约翰斯顿Jr.(E.Russell Johnston Jr.).工程矢量力学(静力学)[M].北京:机械工业出版社,2003.
  • 2张志涌.精通MATLAB6.5版[M].北京:北京航空航天大学出版社,2003..
  • 3M.Shigehara and A.Ohtaka,A Construction Methodology of the Large Solar Array System of a Solar Power Satellite[Z].Dept.of Aerospace Engineering,Tokyo Metropolitan Institute of Technology,Japan,1996.

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