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
