[1] 詹亚锋,马正新.现代微小卫星技术及发展趋势[J].电子学报,2000,28(7):102-106. ZHAN Ya-feng, MA Zheng-xin. Technology of modern micro satellite and its development direction[J]. Acta Electronica Sinica, 2000, 28(7):102-106.
[2] 高彬.小卫星技术的发展现状及其军事应用前景[J].天津通信技术, 2003(2):6-9. GAO Bin. Developing actuality tactic and militaryapplication foreground of small satellite technology[J]. Tianjin Communications Technology, 2003(2):6-9.
[3] 周斌,王劲东.卫星磁部件分布对梯度法消除剩磁的影响分析[J].中国空间科学技术,2013,33(5):29-34. ZHOU Bin, WANG Jin-dong. Influence of magnetic component distribution of satellite on eliminating remanant magnetic field by gradient method[J]. Chinese Space Science and Technology, 2013, 33(5):29-34.
[4] 李杨,涂歆滢.星体剩磁矩对姿控系统影响的仿真研究[J].系统仿真学报,2002,14(2):215-218. LI Yang, TU Xin-ying. Simulation of the remanence moment influencing on satellite attitude control system[J]. Journal of System Simulation, 2002, 14(2):215-218.
[5] HAN K, WANG H, XIANG T, et al. Magneto-meter compensation scheme and experimental results on ZDPS-1A pico-satellite[J]. Chinese Journal of Aeronautics, 2012, 25(3):430-436.
[6] 向甜,王昊,蒙涛,等.三轴磁强计与MEMS陀螺的在轨实时标定方法[J].浙江大学学报:工学版,2014,48(3):541-547. XIANG Tian, WANG Hao, MENG Tao, et al. Real-time on-orbit calibration method for three-axis magnetometer and MEMS gyroscope[J]. Journal of Zhejiang University:Engineering Science, 2014, 48(3):541-547.
[7] INAMORI T, SAKO N, NAKASUKA S. Magnetic dipole moment estimation and compensation for an accurate attitude control in nano-satellite missions[J]. Acta Astronautica, 2011, 68(11):2038-2046.
[8] CRASSIDIS J I, LAI K L, HARMAN R R. Real-time attitude-independent gyro calibration from three-axis magnetometer measurements[C]//AIAA/AAS Astrodynamics Specialist Confe-rence and Exhibit. Providence:AIAA, 2004:1-11.
[9] 段方,刘建业,李丹.微小卫星太阳敏感器/磁强计实时标定算法研究[J].航空学报,2007,28(1):173-176. DUAN Fang, LIU Jian-ye, LI Dan. Real-time sun-sensor/magnetometer calibration algorithm for micro-satellite[J]. Acta Aeronautica et Astro-nautica Sinica, 2007, 28(1):173-176.
[10] 郁丰,刘建业,熊智,等.微小卫星剩磁在轨标定技术研究[J].航空学报,2007,28(5):1142-1145. YU Feng, LIU Jian-ye, XIONG Zhi, et al. Research on remanence on-orbit calibration for micro-satellites[J]. Acta Aeronautica et Astronautica Sinica, 2007,28(5):1142-1145.
[11] 李烨,郁丰,王群仰,等.立方星剩磁在轨辨识与主动补偿技术[J].中国惯性技术学报,2016,24(3):342-348. LI Ye, YU Feng, WANG Qun-yang, et al. On-orbit estimation and compensation for CubeSats reman-ence[J]. Journal of Chinese Inertial Technology, 2016, 24(3):342-348.
[12] 郁丰,刘建业,熊智,等.微小卫星姿态确定系统多信息融合滤波技术[J].上海交通大学学报,2008, 42(5):831-835. YU Feng, LIU Jian-ye, XIONG Zhi, et al. Multi-information fusion method of micro satellite attitude determination system[J]. Journal of Shanghai Jiao Tong University, 2008, 42(5):831-835.
[13] SAKAI S I, FUKUSHIMA Y, SAITO H. Design and on-orbit evaluation of magnetic attitude control system for the "REIMEI" microsatellite[C]//IEEE International Workshop on Advanced Motion Control. Trento:IEEE, 2008:584-589.
[14] 黄琳,荆武兴.关于剩磁对卫星姿态确定与控制影响的研究[J].航空学报,2006,27(3):390-394. HUANG Lin, JING Wu-xing. Effects of remanence on attitude determination and control of satellites[J]. Acta Aeronautica et Astronautica Sinica, 2006, 27(3):390-394.
[15] RONG S, MU R, CUI N. A fault tolerant filter applied on magnetometer-based autonomous satellite navigation[C]//International Symposium on Systems and Control in Aerospace and Astronautics. Harbin:ISSCAA, 2006:597-600.
[16] 章仁为.卫星轨道姿态动力学与控制[M].北京:北京航空航天大学出版社,1998:340-345.
[17] CHUI C K, CHEN G. Kalman filtering with real-time applications[M]. Springer-Verlag, 1987:232-234.
[18] CRASSIDIS J L, Lai K L, HARMAN R R. Real-time attitude-independent three-axis magnetometer calibration[J]. Journal of Guidance Control and Dynamics, 2005, 28(1):115-120. |