摘要
介绍了某飞行器姿态控制系统数字仿真的实现。根据该姿控系统的组成,以俯仰通道为例建立了通道的动力学和运动学方程,以及相应的控制系统数学模型,给出了仿真流程。仿真结果表明:该仿真系统可定量分析飞行器控制系统参数超差对飞行的影响。
The digital simulation implement of attitude control system for some aircraft was introduced in this paper.The dynamic and kinematic equations of the pitching channel which served as an analysis example,and relative models of the control system were established according to the attitude control system.The simulation flowchart was also given out.The simulation results showed that this system would analyze the influence of the parameters of the control system that were overrun tolerance quantitatively on the ...
出处
《上海航天》
北大核心
2008年第1期51-56,共6页
Aerospace Shanghai
关键词
飞行器
姿态控制系统
状态空间
龙格库塔法
阿达姆斯算法
参数超差
Aircraft
Attitude control system
State space
Runge-Kutte method
Adams method
Parameter overrun tolerance
