摘要
为了实现在整星制约条件下,以经济而可靠的手段满足三轴稳定多任务微小卫星(MTMS)姿态控制系统的功能和性能要求,分析了MTMS的运行任务,提出了基于多任务要求的工作模式划分,并对多任务过程的姿态确定和姿态控制系统进行综合分析和设计,建立数学模型。通过仿真验证,可实现多任务微小卫星的复杂任务设计要求。
Under the constraint conditions of the whole satellite, in order to meet the functions and performance requirements of the three-axis stabilized multi-task micro-satellite （MTMS） attitude control system through economic and reliable means, the operation tasks of MTMS are analyzed, the operating mode division based upon multi-mission requirements is raised, the attitude determination and attitude control system in the multi-task process are analyzed comprehensively, and a mathematical model is established. By simulation experiment, the design requirements of complex tasks of multi-mission micro-satellite can be achieved.
出处
《系统仿真学报》
CAS
CSCD
北大核心
2010年第A01期39-42,共4页
Journal of System Simulation
关键词
多任务
三轴稳定
工作模式
姿态确定
姿态控制
multi-task
three-axis stabilized
operating mode
attitude determination
attitude control
