摘要
本文论述了运载火箭三通道大姿态调姿系统的设计和数学仿真。首先建立了箭体全量、三通道运动模型，接着介绍了用多变量系统现代频域理论，进行调姿系统设计的基本思想和方法，最后以实例给出了系统设计和数学仿真结果。
This paper describes the design and mathematical simulation of the three-axis attitude-adjusting system of launch vehicle. First, the models of launch vehicle and its three-axis motion are built, and then the basic ideology and method of designing attitude-adjusting system by modern frequency domain theory of multivariable system are presented. Finally, the results of system design and mathematical simulation of actual models are given.
出处
《导弹与航天运载技术》
1994年第4期15-22,共8页
Missiles and Space Vehicles
关键词
运载火箭
姿态控制
数学模拟
Launch vehicle, Attitude control, Mathematical simulation.
