基于高斯伪谱法的碰撞规避策略研究

安喜彬; 何兵; 陈福贵; 刘炳琪; 林浩申

doi:10.11728/cjss2017.02.202

基于高斯伪谱法的碰撞规避策略研究

doi: 10.11728/cjss2017.02.202

1. 第二炮兵工程大学空间工程系西安 710025;
2. 96669部队北京 102208

基金项目:

国家自然科学基金项目（61403399）和陕西省基金项目（2015JQ6213）共同资助

详细信息

作者简介:
安喜彬,E-mail:anxb029@163.com

中图分类号: V412.4
计量
- 文章访问数: 821
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- 被引次数: 0
出版历程
- 收稿日期: 2016-01-18
- 修回日期: 2016-11-01
- 刊出日期: 2017-03-15

Collision avoidance strategies based on Gauss pseudospectral method (in Chinese)

1. Department of Aerospace Engineering, The Second Artillery Engineering University, Xi'an 710025;
2. 96669 Troops, Beijing 102208

摘要

摘要: 为保证在轨卫星运行安全，对于碰撞概率较高的空间交会情况需要进行规避机动，防止在轨卫星与空间碎片碰撞.选取连续推力策略进行规避机动，将空间碰撞规避过程转化为满足复杂约束的最优控制问题，采用高斯伪谱法对最优控制律进行求解，求解结果满足相应约束.研究结果为航天器有效规避空间碰撞威胁提供了有力支持.
- 高斯伪谱 /
- 空间碎片 /
- 空间碰撞 /
- 规避策略
Abstract: In order to ensure the safety of active satellite, it is necessary to perform an orbit maneuver before the collision between space debris and satellite to protect satellite from space debris. The strategy of continuous-thrust is chosen for avoiding collision. The collision avoidance process is converted to optimal control problem with complicated constraints, while Gauss pseudospectral method is used to solve this problem and the result meets the requirements of avoidance. The simulation results show that the new method can decrease the consumption of fuel. It is significant for avoiding collision between space debris and the satellite.
- Gauss pseudospectral method /
- Space debris /
- Space collision /
- Avoidance strategies

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参考文献(13)

[1]	WANG Jianfeng, LIU Jing, LIU Lin. On research of the evadible period and satellite orbit maneuver[J]. Chin. J. Space Sci., 2009, 29(2):234-239(王建峰, 刘静, 刘林. 规避时段选择与机动变轨研究[J]. 空间科学学报, 2009, 29(2):234-239)
[2]	GUO Rong. Study on Space Debris Collision Early Warning and Maneuver Strategy to Low Earth orbit Spacecraft[D]. Changsha:National University of Defense Technology, 2005:35-55
[3]	WANG Xiaowei, LIU Jing. Space objects long-term evolution model and the first analysis[C]//the 8th International Conference of Space Debris. Beijing:Beijing Institute of Technology, 2015:238-241
[4]	BROADNAX A D. Debris Avoidance Strategies for Spacecraft[D]. San Jose:San Jose State University, 2001:20-83
[5]	MASON J, STUPL J, MARSHALL W, et al. Orbital debris-debris collision avoidance[J]. Adv. Space Res., 2011(48):1643-1655
[6]	ABDEL-AZIZ Y A. An analytical theory for avoidance collision between space debris and operating satellites in LEO[J]. Appl. Math. Model., 2013(36):8283-8291
[7]	ALFANO S. Satellite collision probability enhancements[J]. J. Guid. Control Dyn., 2006, 29(2):588-593
[8]	ZHENG Qinyu, WU Lianda. A computation method to warn the collision event between space probe and debris[J].Acta Astron. Sin., 2004, 45(4):422-430
[9]	YANG Liang, ZHENG Zonggui, XU Heng, et al. Onboard Gauss pseudo spectral terminal guidance law with multiple constraints[J]. J. Ballist., 2014, 26(3):98-104
[10]	SHANG Haibin, CUI Pingyuan, XU Rui et al. Fast optimization of interplanetary low-thrust transfer trajectory based on Gauss pseudospectral algorithm[J]. J. Astron., 2010, 31(4):1001-1012
[11]	BENSON A, THORVALDSEN T. Direct trajectory optimization and costate estimation via an orthogonal collocation method[J]. J. Guid. Control Dyn., 2006, 29(6):1435-1440
[12]	HUNTINGTON G T. Advancement and Analysis of a Gauss Pseudospect Ralt Ranscription[D]. Cambridge, MA:Massachusetts Institute of Technology, 2007
[13]	HU Chen. Research on Algorithm of Tracking Satellite Applying Space-Based Bearing-Only Measurement Based on CKF[D]. Xi'an:The Second Artillery Engineering University, 2013