摘要
本文就全轨道实时星模拟器的设计及实现方法进行了深入的研究，提出了能满足卫星控制系统半物理仿真用的星模拟器设计方案；讨论了星图生成器选择依据；模拟器光学系统设计原则；系统精度的实现及误差修正方法等问题。
This paper makes a through study in the method of designing and realizing whole-orbitreal-time star simulator and advances the design plan of star simulator which can meet the requirement ofhardware-in-the-loop simulation of satellite attitude control system. Several questions about selecting thestar displayer,determining the design principle of optical system of simulator,realizing the system preci-sion and correcting the system error are also discussed in this paper.
出处
《系统仿真学报》
CAS
CSCD
1995年第2期40-45,共6页
Journal of System Simulation
关键词
星模拟器
仿真
姿态控制系统
卫星
Hardware-in-the-loop simulation Whole-orbit real-time star simulator Simulation
