Control of space station and its adjoint orbiter using relative DGPS

被引：0
|
作者：
Yuan, JP [1 ]
Luo, JJ [1 ]
Dou, XM [1 ]
Tian, ZY [1 ]
机构：
[1] Northwestern Polytech Univ, Coll Astronaut, Xian 710072, Peoples R China
来源：
SPACEFLIGHT MECHANICS 1998, VOL 99, PTS 1 AND 2 | 1998年 / 99卷
关键词：
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The control of space station and its adjoint orbiter is theoretically the control of relative motion of two or more space vehicles, including relative dynamics, relative kinematics, and relative attitude. Relative GPS can be used to navigating a vehicle in the vicinity of its target or destination. In this paper, GPS/DGPS are introduced and relative motion of space vehicles are modeled. Relative position, relative velocity and relative attitude are represented and solved by GPS/DGPS measurements. Use of some type of commercial GPS receiver onboard spacecraft and relative differential GPS technique, the relative attitude of space station and its adjoint satellite can be accurately calculated in real-time.
引用
收藏
页码：1383 / 1389
页数：7
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