基于飞行器姿态控制系统的导引头跟踪实验  

Seeker tracking experiment based on spacecraft attitude control system

作　　者：王佳伟[1] 杨亚非[1] 钱玉恒[1] 

机构地区：[1]哈尔滨工业大学飞行器控制实验教学中心,黑龙江哈尔滨150001

出　　处：《实验技术与管理》2015年第6期120-122,126,共4页Experimental Technology and Management

基　　金：黑龙江省教学研究项目(JG2013010268)

摘　　要：为形象地模拟导弹跟踪目标时的姿态控制和调整过程,提高学生对于飞行器控制课程的理解,开发了飞行器姿态控制系统的导引头跟踪实验。介绍了实验系统的组成,包括硬件结构和软件平台;阐述了导引头跟踪目标实验的原理,分别验证了在目标静止和运动情况下,导引头对目标进行跟踪的效果,并且得到了仿真图形。The spacecraft attitude control system can simulate the process of attitude control and adjustment of missile while tracking target,trod improve the students＇ understanding of the courses for spacecraft control. Firstly, the structure of the experimental system is introduced, including the hardware structure and software platform.and then the principle of seeker tracking target experiment is explained. Finally, the effect of seeker tracking to the target is verified through the target stationary and mobile cases, and simulation graphics are given

关 键 词：飞行器姿态控制系统 导引头 目标跟踪 

分 类 号：TP271[自动化与计算机技术—检测技术与自动化装置]