摘要
围绕中继卫星应用于航天发射测控的跟踪控制技术,重点研究了对运载火箭的高精度指向控制计算方法,并通过对仿真发射弹道的模拟跟踪,完成了中继卫星星间天线对运载火箭高精度的跟踪指向控制计算。研究表明采用中继卫星系统可以完成对运载火箭的高精度指向跟踪任务,满足航天发射测控任务需求。
In this paper, the tracking computation approach of precious pointing control for TDRS tracking space launch vehicle is studied. Through the calculation of a specific simulated ballistic trajectory, the pointing control calculation task of IOLA （the inter-orbit link antenna） of TDRS tracking space launch vehicle is completed. It shows that the pointing control task of supporting space launch can be accomplished with TDRS. The research on pointing computation model for IOLA of TDRS tracking space launch vehicle would benefit for lasting and continuous space TT＆C of space launch vehicle.
出处
《载人航天》
CSCD
2010年第4期24-29,共6页
Manned Spaceflight
