Dynamics Analysis of Lager Spacecraft
With Deploying Flexible Appendages
Ma Xingrui
(China Aerospace Science and Technology Corporation,Beijing 100830) Wang Tianshu Wang Benli Kong Xianren
(Harbin Institute of Technology,Harbin 150001)
Abstract The several important problems such as deployment procedure of flexible appendages on complex spacecraft are analyzed,and corresponding programme and application software are introduced.Appendages deployment is analyzed by numerical simulation.The contents including attitude motion,attitude velo city,deployment and vibration of flexible appendages etc are discussed.
Subject Term Flexible body Spacecraft Dynamic simulation Analyzing