摘要
分析了大型飞行器动态飞行控制系统的数学模型，给出了其仿真系统的基本构成方案，并对制导与姿态控制的联合六自由度仿真。
The mathematical model of space vehicle dynamic flying control system is analyzed. The basic composition of the simulation system is presented. The six degrees of freedom simulation of guidance and stability, the object oriented simulation modeling method and the integrated simulation software structure are studied.
出处
《计算机仿真》
CSCD
1999年第1期34-36,共3页
Computer Simulation
关键词
飞行器
仿真
飞行控制系统
姿态控制
Space vehicle Control system Simulation Object oriented Integrated
