摘要
在挠性卫星的控制仿真系统设计中,卫星的动力学模型多根据数学方程搭建.此处介绍一种以虚拟样机技术为基础,以ADAMS、MATLAB软件为核心平台的航天器动力学建模与控制方法。揭示了此种方法的可行性与优越性,详细介绍了此种方法的流程,并以三轴零动量反作用飞轮控制的挠性卫星为例进行了检验。
In the design of control and simulation system of flexible satellite, the dynamic model of satellite was built based on mathematic function mostly. A new method based on virtual prototype technology was proposed. With this method, the modeling and control of flexible satellite are based on the ADAMS and MATLAB. The feasibility and advantages about the method were revealed, and the main process about it was introduced in detail. A case about flexible satellite controlled by three-axis zero momentum reaction flywheel validates the effect of the method.
出处
《系统仿真学报》
CAS
CSCD
北大核心
2009年第2期590-593,598,共5页
Journal of System Simulation
