应用信标模式测速的实现方法及论证  

Range Rate Measurement with Beacon Signals

作　　者：李雪光[1] 贾兴泉 师振荣 王国平[1] 张瑞国[1] 

机构地区：[1]太原卫星发射中心,山西太原030027

出　　处：《飞行器测控学报》2006年第2期37-43,共7页Journal of Spacecraft TT&C Technology

摘　　要：根据未来固体火箭型号试验越来越多，首区无线电设备受火箭尾焰干扰的情况以及测控体制的发展要求，探讨了利用信标模式[1]进行高精度测量时所面临的工程问题，包括信标模式下测量值的误差项分析，减小测量误差的方法等内容。More and more solld-state rockets will be used and radio equipment at launch sites are encountering more and more interference from rocket plume. To meet requirements for development of TT＆C systems, the paper discusses issues in engineering for high-precision measurement of range rate with beacon signals. Analysis of error items in measurements and the method to reduce measurement errors are also given.

关 键 词：信标模式 测量误差 相干系统 

分 类 号：V556[航空宇航科学与技术—人机与环境工程]