Alternative TitleSpace microgravitycombination and its control
Source Publication中国空间科学技术
Volume39Issue:5Pages:49-54; AR:1000-758X(2019)39:5<49:KJWZLZ>2.0.TX;2-3
Keyword空间组合体 微重力环境 绳系卫星系统 航天器交会对接 距离速率控制算法 space combination microgravity environment tethered satellite system rendezvous and docking range rate control algorithm
Other AbstractSpace microgravity combination is an upgraded version of the tethered satellite system, a more powerful and prospective version for future applications.However,both the systems are beset with the same problem:if there is no preset control,the system's motion is unstable. Therefore,an effective control algorithm has to be developed to make the system stable.Based on a simplified dynamic model of tethered satellite,the relationship between microgravity and dynamic inertia forces was used to deduce a very unique range rate control algorithm to stabilize the system concisely and productively.This algorithm can be applied to mass-distributed,elastic and other more complex cases of tethered satellite control.It can also be successfully adopted to control in-orbit rendezvous and docking missions of the space microgravity combination.
Indexed ByCSCD
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Cited Times:1[CSCD]   [CSCD Record]
Document Type期刊论文
Affiliation1.于绍华, 中国科学院国家空间科学中心, 北京 100080, 中国.
2.Yu Shaohua, National Space Science Center,Chinese Academy of Sciences, Beijing 100080, China.
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于绍华. 空间微重力组合体及其控制[J]. 中国空间科学技术,2019,39(5):49-54; AR:1000-758X(2019)39:5<49:KJWZLZ>2.0.TX;2-3.
APA 于绍华.(2019).空间微重力组合体及其控制.中国空间科学技术,39(5),49-54; AR:1000-758X(2019)39:5<49:KJWZLZ>2.0.TX;2-3.
MLA 于绍华."空间微重力组合体及其控制".中国空间科学技术 39.5(2019):49-54; AR:1000-758X(2019)39:5<49:KJWZLZ>2.0.TX;2-3.
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