摘要
为满足航天器姿态控制系统仿真的需要 ,利用面向对象建模方法 ,设计了受控航天器的通用仿真框架。在该框架中 ,航天器、姿态表示、控制律、执行机构作为独立的对象建模 ,可以支持不同仿真背景、不同粒度下的仿真要求。利用该框架建立的飞船姿态控制系统仿真模型 。
Using object-oriented modeling method,a general simulation frame is designed in order to meet the needs of the attitude control system simulation for spacecraft. In the frame,spacecraft, attitude expressions, control laws and actuators are modeled as independent classes,so the frame can support attitude control system simulation with various backgrounds and various grains. The effectiveness of the frame is validated by a spaceship′s attitude control simulative models built by the frame.
出处
《航天控制》
CSCD
北大核心
2001年第1期67-70,74,共5页
Aerospace Control
