Trajectory Design and Simulation of Space-Based Surveillance Controlled Flying Around for GEO Slow-Spinning Space Target

被引：0
|
作者：
Zhang Y. [1 ,2 ]
Gan Q.-B. [3 ]
Fu J.-L. [1 ]
Li Z.-S. [1 ]
Yuan H. [1 ]
Xiong Y. [1 ,2 ]
机构：
[1] Academy of Opto-Electronics, Chinese Academy of Sciences, Beijing
[2] University of Chinese Academy of Sciences, Beijing
[3] National Astronomical Observatories, Chinese Academy of Sciences, Beijing
来源：
| 1600年 / Beijing Institute of Technology卷 / 40期
关键词：
Controlled flying around; Multi-pulse control; Relative motion; Slow-spinning space target; Spiral approaching;
D O I：
10.15918/j.tbit1001-0645.2018.534
中图分类号：
V27 [各类型航空器]; V24 [航空仪表、航空设备、飞行控制与导航];
学科分类号：
082503 ;
摘要：
A method of controlled flying around of space-based surveillance was proposed to observe continuously the specific surface of GEO slow-spinning space target. Firstly, a relative motion model of target and space-based platform was established. And then, analyzing the expected relative orbit model of arbitrary spin axis, a single cycle controlled flying around model and a multi-cycle spiral approaching controlled flying around model were designed. Time constrained multi-pulse control was used to realize controlled flying around. Finally, the controlled flying around orbit with different flying radius, different number of pulses and different flying periods was simulated and analyzed to provide and verify a multi-cycle spiral approaching controlled flight strategy. The results show that, by mapping the attitude changes of GEO slow-spinning space target to the design of relative controlled flying around orbit, the continuous surveillance of the specific surface can be realized. The simulation results and conclusions can provide a significant reference for engineering application. © 2020, Editorial Department of Transaction of Beijing Institute of Technology. All right reserved.
引用
收藏
页码：441 / 447
页数：6
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