Please wait a minute...
浙江大学学报(工学版)
J4  2010, Vol. 44 Issue (9): 1719-1723    DOI: 10.3785/j.issn.1008-973X.2010.09.015
无线电电子学、电信技术     
基于太阳能电池板的皮卫星最优姿态确定算法
韩柯,金仲和,王昊
浙江大学 信息与电子工程学系,浙江 杭州 310027
Optimal attitude determination method for
 pico-satellite using solar panels
HAN Ke, JIN Zhong-he, WANG Hao
Department of Information and Electronics Engineering, Zhejiang University, Hangzhou 310027, China
 全文: PDF 
摘要：

为了提高皮卫星系统的设计冗余和可靠性,太阳能电池板可以复用为粗太阳敏感器.由于具有全空间视场,这一灵活的配置对周边光源有较强的敏感性,因此,在地球反照光干扰下,测量精度不高.在这一特定情况下,研究了改进的姿态确定算法,以提高卫星的姿态测量精度.根据反照光影响下电池板的实际输出情况,重新讨论Wahba问题,提出太阳能电池板定姿的新损失函数,并推导了该函数最小二乘意义下的最优姿态确定方法.与基于Wahba模型常用的四元素估计法（QUEST）相比,该模型的定姿算法具有更高的精度.蒙特卡罗仿真表明：该算法的平均定姿误差比QUEST小17%,误差标准差比QUEST小57%．
关键词： 皮卫星;  太阳能电池板;  姿态确定;  最小二乘问题    
Abstract:

Solar panels can also be used as coarse sun sensors to increase the pico-satellite system’s redundancy and reliability. This flexible setup is easily sensitive to surrounding light sources as it sees the whole sky, so with the interference of Earths albedo light, it does not show a high accuracy. To improve the performance of satellite attitude measurement in this specific situation, a modified attitude determination method was investigated. According to the actual output of solar panel with the interference of albedo light, the Wahbas problem was re-discussed, and a new loss function for optimal attitude determination was proposed. Also the method to solve the optimal weighted leastsquare function was developed. From simulation, compared with the classic quaternion estimator (QUEST), which is based on Wahbas loss function, the suggested attitude determination method, which is based on the new loss function, shows higher accuracy. Monte Carlo simulation shows that the average attitude error of the suggested method is 17% lower than QUEST, and the standard deviation is 57% lower as well．
Key words: pico-satellite    solar panels    attitude determination    least-square problem
出版日期: 2010-10-10
:     
基金资助:

中国博士后科学基金资助项目（20080431306）；中国博士后科学基金特别资助项目（20081458）；教育部新世纪优秀人才支持计划资助项目（NCET-06-051）；高等学校全国优秀博士学位论文作者专项资金资助项目（200035）.
作者简介: 韩柯（1984-），男，陕西西安人，博士生.从事皮卫星姿态测量及控制系统设计研究.E-mail: ZJUHank@gmail.com
服务　　
把本文推荐给朋友
加入引用管理器
E-mail Alert
RSS
作者相关文章　　
韩柯
金仲和
王昊

引用本文:

韩柯, 金仲和, 王昊. 基于太阳能电池板的皮卫星最优姿态确定算法[J]. J4, 2010, 44(9): 1719-1723.

HAN Ke, JIN Zhong-He, WANG Hao. Optimal attitude determination method for
 pico-satellite using solar panels. J4, 2010, 44(9): 1719-1723.

链接本文:

http://www.zjujournals.com/xueshu/eng/CN/10.3785/j.issn.1008-973X.2010.09.015    或    http://www.zjujournals.com/xueshu/eng/CN/Y2010/V44/I9/1719

［1］ HEIDT H, PUIGSUARI J, MOORE A S, et al. Cubesat: a new generation of picosatellite for education and industry lowcost space experimentation ［C］∥ 14th Annual AIAA/USU Conference on Small Satellites. Logan, Utah, USA: AIAA/USU, 2000: 113116．
［2］ 刘建业,段方,李丹,等.基于太阳电池板与磁强计的小卫星姿态确定算法研究［J］.宇航学报,2007,28(1): 218222.
LIU Jianye, DUAN Fang, LI Dan, et al. An algorithm for microsatellite attitude determination using solar panels and magnetometer ［J］. Journal of Astronautics, 2007,28(1): 218222．
［3］ APPEL P. Attitude estimation from magnetometer and earthalbedocorrected coarse sun sensor measurements ［J］. Acta Astronautica, 2005, 56(1/2): 112．
［4］ SHUSTER M D, OH S D. Threeaxis attitude determination from vector observations ［J］. Journal of Guidance, Control, and Dynamics, 1984,4(1): 7077．
［5］ MARKLEY F  L. Attitude determination using vector observations: a fast optimal matrix algorithm ［J］. Journal of the Astronautical Sciences, 1993,41(2): 261280．
［6］ MORTARI D. ESOQ: A Closeform solution to the Wahaba problem ［J］. Journal of the Astronautical Sciences, 1997,45(2): 159204．
［7］ MORTARI D. Second estimator for the optimal quaternion ［J］. Journal of Guidance, Control, and Dynamics, 2000,23(1): 885888．
［8］ WAHBA G. A leastsquare estimate of satellite attitude ［J］. SIAM Review, 1965,7(3): 409．
［9］ 赵翔宇,金小军,韩柯,等.皮卫星电源系统的设计与仿真［J］.浙江大学学报:工学版,2009,43(2):228233．
ZHAO Xiangyu, JIN Xiaojun, HAN Ke, et al. Design and simulation of the power system of picosatellite ［J］. Journal of Zhejiang University: Engineering Science, 2009,43(2): 228233．
[1] 吴昌聚,徐秀琴. 基于导轨结构的新型笼式皮卫星分离机构[J]. J4, 2014, 48(3): 548-554.
[2] 吴昌聚, 徐秀琴. 皮星1号A卫星（ZDPS-1A）被动热控制技术[J]. J4, 2013, 47(8): 1450-1456.
[3] 向甜,王昊,蒙涛,韩柯,金仲和. 基于纯磁控的皮卫星姿态恢复[J]. J4, 2013, 47(5): 843-852.
[4] 丁立聪,金小军,王春晖,金仲和. ZDPS-1A卫星电源系统设计与在轨验证[J]. J4, 2012, 46(11): 2073-2080.
[5] 杨牧, 王昊, 张钰, 郑伟, 郑阳明, 金仲和. 抗辐射加固的皮卫星用实时操作系统设计[J]. J4, 2011, 45(6): 1021-1026.
[6] 韩柯, 王昊, 朱小丰, 向甜, 金仲和. 皮卫星偏置动量轮在轨备份切换策略[J]. J4, 2011, 45(10): 1771-1776.
[7] 金小军, 赵翔宇, 辜渝嘉, 等. 皮卫星在轨能量平衡仿真研究[J]. J4, 2009, 43(7): 1282-1287.
[8] 赵翔宇 金小军 韩柯 金仲和. 皮卫星电源系统的设计与仿真[J]. J4, 2009, 43(2): 228-233.