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返回式卫星回收系统的控制问题
引用本文:李颐黎.返回式卫星回收系统的控制问题[J].中国空间科学技术,1990,10(6):30-33,43.
作者姓名:李颐黎
作者单位:北京机电研究设计所
摘    要:从一假想的卫星的返回轨道分析出发,论述了返回式卫星回收系统的“过载一时间”控制方案,说明了该方案是无人卫星回收的一种简便的、可行的控制方案。建议对某些卫星采用长的抛罩后的滑行段,以降低开伞马赫数及速压。

关 键 词:卫星  返回式  回收系统  控制  着陆

CONTROL OF RECOVERY SYSTEM OF RETURNABLE SATELLITE
Li Yili.CONTROL OF RECOVERY SYSTEM OF RETURNABLE SATELLITE[J].Chinese Space Science and Technology,1990,10(6):30-33,43.
Authors:Li Yili
Institution:Beijing Institute of Space Mechine and Electricity
Abstract:In this paper, a "overload-time" control program of returnable satellite is discussed on the basis of the return trajectory analyses for a imaginary satellite. It is explained that this control program is simple and feasible for the recovery of unmanned satellite.In this paper, it is proposed that a longer non-therm-shield coast flight phase can be adopted for some satellites in order to reduce the Mach number and the dynamic pressure when the parachute is employed.
Keywords:Recoverable satellite  Spacecraft recovery  Landing control
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