Browse > Article
http://dx.doi.org/10.5139/JKSAS.2014.42.12.1020

Suitability of Singularity Indices for Steering Law Design of Control Moment Gyros  

Jin, Jaehyun (Sunchon National University)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.42, no.12, 2014 , pp. 1020-1027 More about this Journal
Abstract
Singularity indices for steering law design of CMGs have been analyzed. Several qualitative criteria to evaluate the suitability of indices have been suggested. Fast calculation and consistency with the condition number of the input matrix are the most important ones. Based on these criteria, modified indices have been proposed. Properties of infinite value and finite value indices have been compared and an ad hoc method to combine those properties has been presented. Computer simulation results are given to verify the proposed method.
Keywords
Control moment gyros; Singularity avoidance; Singularity index; Determinant;
Citations & Related Records
Times Cited By KSCI : 3  (Citation Analysis)
연도 인용수 순위
1 Lappas, V., et al., "Design and testing of a control moment gyroscope cluster for small satellites," Journal of Spacecraft and Rockets, vol.42, no.4, pp.729-739, 2005.   DOI
2 Lapas, V., et al., "Laboratory experiments of a control moment gyroscope cluster for agile small satellites," Proceedings of the 5th International ESA Conference on Spacecraft Guidance, Navigation and Control Systems, pp. 109-113, 2002.
3 Rhee, S. and Kwon, H., "Low cost small CMG performance test and analysis," Journal of The Korean Society for Aeronautical and Space Sciences, Vol.39, No.6, 2011, pp.543-552.   과학기술학회마을   DOI   ScienceOn
4 Lee, S., "Technology of control moment gyroscope and its industrial trend," Journal of The Korean Society for Aeronautical and Space Sciences, Vol.40, No.1, 2012, pp.86-92.   과학기술학회마을   DOI   ScienceOn
5 Oh, H. and Vadali, S., "Feedback control and steering laws for spacecraft using single gimbal control moment gyros," The Journal of the Astronautical Sciences, Vol. 39, No. 2, 1991, pp.183-203.
6 Wie, B., Bailey, D., and Heiberg, C., "Singularity robust steering logic for redundant single-gimbal control moment gyros," Journal of Guidance, Navigation, and Control, Vol.24, No.5, 2001, pp.865-872.   DOI   ScienceOn
7 Ford, K. and Hall, C., "Singular direction avoidance steering for control moment gyros," Journal of Guidance, Navigation, and Control, Vol.23, No.4, 2000, pp.648-656.   DOI   ScienceOn
8 Schaub, H. and Junkins, J., "Singularity avoidance using null motion and variable-speed control moment gyros," Journal of Guidance, Navigation, and Control, Vol.23, No.1, 2000, pp.11-16.   DOI   ScienceOn
9 Jang, W., Rhee, S., and Kwon, H., "Development of 0.6Nm small CMG hardware and performance test," Journal of The Korean Society for Aeronautical and Space Sciences, Vol.38, No.9, 2010, pp.933-942.   과학기술학회마을   DOI   ScienceOn
10 Kurokawa, H., "Survey of theory and steering laws of single-gimbal control moment gyros," Journal of Guidance, Navigation, and Control, Vol.30, No.5, 2007, pp.1331-1340.   DOI
11 Lee, H., Lee, I., and Bang, H., "Optimal steering laws for variable speed control moment gyros," AIAA Guidance, Navigation, and Control Conference and Exhibit, SF, CA, AIAA Paper 2005-6395, Aug., 2005, pp.5368-5378.
12 Leeghim, H., Bang, H., Park, J., "Singularity avoidance of control moment gyros by one-step ahead singularity index," Acta Astronautica, Vol. 64, No.9-10, 2009, pp.935-945,   DOI   ScienceOn
13 McMahon, J. and Schaub, H., "Simplified singularity avoidance using variable speed control moment gyroscope null motion," Journal of Guidance, Navigation, and Control, Vol.32, No.6, 2009, pp.1938-1943.   DOI
14 Cui, P. and He, J., "Steering law for two parallel variable speed double gimbal control moment gyros," Journal of Guidance, Navigation, and Control, Vol.37, No.1, 2014, pp.350-359.   DOI