Optics and Precision Engineering, Volume. 20, Issue 5, 1031(2012)
Staring imaging attitude tracking control of agile small satellite
[1] [1] TU SH CH. Dynamics and Control of Satellite attitude[M]. Beijing: China Astronautic Publishing House, 2006: 266-267. (in Chinese)
[2] [2] LEEGHIMA H, BANG H, PARK J. Singularity avoidance of control moment gyros by one-step ahead singularity index [J]. Acta Astroautica, 2009,64(9-10): 935-945.
[3] [3] WIE B, HEIBERG C, BAILEY D. Singularity robust steering logic for redundant single-gimbal control moment gyros [J]. Journal of Guidance Control and Dynamics, 2001, 24(5): 865-872.
[4] [4] WIE B. Singularity analysis and visualization for single-gimbal control moment gyro systems [J]. Journal of Guidance, Control, and Dynamics, 2004, 27 (2): 271-282.
[5] [5] YOON H, TSIOTRAS P. Singularity analysis of variable-speed control moment gyros [J]. Journal of Guidance, Control, and Dynamics, 2004, 27 (3): 374-386.
[6] [6] FORD K A, HALL C D. Singular direction avoidance steering for control-moment gyros[J]. Journal of Guidance, Control, and Dynamics, 2000, 23(4): 648-656.
[7] [7] RICHIE D J, LAPPAS V J. Practical steering law for small satellite energy storage and attitude control [J]. Journal of Guidance, Control, and Dynamics, 2009, 32(6): 1898-1911.
[8] [8] HALL C D. High-speed flywheels for integrated energy storage and attitude control [C]. Proceedings of the American Control Conference, 1997: 1894-1898.
[9] [9] RICHIE D. Combined attitude control and energy storage for small satellites using variable speed control moment gyroscopes [D]. UK: Univ. Of Surrey, 2008.
[10] [10] JIA Y H, XU SH J. Integrated power and attitude control of spacecraft using variable speed control moment gyros [J]. Acta Aeronautica Et Astronautica Sinica, 2007, 28(3): 647-653. (in Chinese)
[11] [11] LAPPAS V, RICHIE D, HALL C, et al. Survey of technology developments in flywheel attitude control and energy storage systems [J]. Journal of Guidance, Control, and Dynamics, 2009, 32(2): 354-365.
[12] [12] WIE B, HEIBERG C, BAILEY D. Rapid multi-target acquisition and pointing control of agile spacecraft [J]. Journal of Guidance, Control, and Dynamics, 2002, 25(1): 96-104.
[13] [13] LAPPAS V J. A Control moment gyro (CMG) based attitude control system (ACS) for agile small satellites [D]. UK: University of Surrey, 2002.
[14] [14] BRADFORD A, GOMES L M, SWEETING M. BILSAT-1: a low-cost, agile, earth observation microsatellite for Turkey [J]. Acta Astronautica, 2003(53): 761-769.
[15] [15] TANG L, XU SH J. Spacecraft adaptive attitude tracking and stable control with variable speed control moment gyroscopes[J]. Acta Aeronautica et Astronautica Sinica, 2006, 27(4): 663-669. (in Chinese)
[17] [17] LAPPAS V J, WIE B. Robust control moment gyroscope steering logic with gimbal angle constraints [J]. Journal of Guidance,Control,and Dynamics, 2009, 32(5): 1662-1666.
[18] [18] ZHANG J R. Estimation of MCMG parameters and torques for rapid slewing maneuver of agile spacecraft [J]. Journal of Tsinghua University (Science and Technology), 2007, 47(11): 2040-2043. (in Chinese)
[19] [19] WU ZH, WU H X. Survey of steering laws for single gimbal control moment gyroscope systems [J]. Journal of Astronautics, 2000, 21(4): 140-145. (in Chinese)
[20] [20] ZHANG J, XU SH J. Singularity analysis and steering law design of IPACS with VSCMGs [J]. Acta Aeronautica Sinica, 2008, 29(1): 123-130. (in Chinese)
[21] [21] KUROKAWA H. Survey of theory and steering laws of single-gimbal control moment gyros [J]. Journal of Guidance, Control, and Dynamics,2007,30(5): 1331-1340.
[22] [22] LAPPAS V, WIE B. Robust CMG steering logic with gimbal angle constraints [C]. AIAA Astrodynamics Specialist Conference and Exhibit, Keystone, CO, Aug, 2006: 1-14.
[23] [23] XING L F, SUN CH Q, TANG L. VSCMGs-based steering law design for a high attitude stability agile satellite [J]. Aerospace Control and Application, 2008, 34(6): 24-28. (in Chinese)
[24] [24] OH H, VADALI S. Feedback control and steering laws for spacecraft using single gimbal control moment gyro [J]. Journal of the Astronautical Sciences, 1991, 39(2): 183-203.
Get Citation
Copy Citation Text
CHEN Xue-qin, GENG Yun-hai, WANG Feng, LI Dong-bai. Staring imaging attitude tracking control of agile small satellite[J]. Optics and Precision Engineering, 2012, 20(5): 1031
Category:
Received: Dec. 2, 2011
Accepted: --
Published Online: Aug. 8, 2012
The Author Email: CHEN Xue-qin (cxqhit@hit.edu.cn)