1 |
Zheng, Z., Yuanqing, X., and Mengyin, F., "Adaptive Sliding Mode Control for Attitude Stabilization With Actuator Saturation," IEEE Tran. on Industrial Electronics, Vol. 58, No. 10, Oct. 2011, pp. 4898-4906
DOI
ScienceOn
|
2 |
Ahn, C., and Kim, Y., "Adaptive BackStepping Sliding Mode Controller for Satellite Control System Using Thrusters," KSAS08-2706, 2008, pp. 934-937
|
3 |
Bing, X., Qinglei, H., and Youmin Z., "Adaptive Sliding Mode Fault Tolerant Attitude Tracking Control for Flexible Spacecraft Under Actuator Saturation," IEEE Tran. on Control Systems Technology, Vol. 20, No. 6, Nov. 2012, pp. 1605-1612
DOI
ScienceOn
|
4 |
Qinglei, H. and Bing X. "Adaptive Fault Tolerant Control Using Integral Sliding Mode Strategy with Application to Flexible Spacecraft," International Journal of Systems Science, 2012, pp. 1-14
|
5 |
Ahn, C., Kim, Y., and Kim H., "Fault Tolerant Flight Control System Design Using Adaptive and Sliding Mode Control Scheme,", KSAS05-1208, 2005, pp. 133-136
|
6 |
Park, Y., Nam, M., Bang, H., "A Study On the Wheel Momonetum Management of Geosynchronous Satellite with Pyramid Constellation of Reaction Wheel," KSAS Fall Conference (1), 2002, pp. 723-727
|
7 |
Bong, W., Spacecraft Dynamics and Control: Applications of Dynamical Systems Theory, AIAA, 1998, pp. 398-401
|
8 |
Bang, H., Tahk, M., and Choi, H., "Large angle attitude control of spacecraft with actuator saturation," Control Engineering Practice, Vol. 11, No. 9, 2003, pp. 989-997
DOI
ScienceOn
|
9 |
Jin, J., Ko, S., and Ryoo, C. K., "Fault tolerant control for satellites with four reaction wheels," Control Engineering Practice, Vol. 16, No. 10, 2008, pp. 1250-1258
DOI
ScienceOn
|
10 |
J. Jin, H. Lee and M. Tahk, "Fault Tolerant Attitude Control for a Spacecraft Using Reaction Wheels," Journal of The Society for Aeronautical and Space Sciences, Vol. 35, No. 6, 2007, pp. 526-532
과학기술학회마을
DOI
ScienceOn
|
11 |
B. T. Costic, D. M. Dawson, M. S. de Queiroz, and V. Kaaila, "A Qauternion-Based Adaptive Attitude Tracking Controller Without Velocity Measurements," Proc. of the 39th IEEE Conference on Decision and Control, Dec. 2000
|
12 |
D. S. Yoo and M. J. Chung, "A Variable Structure Control with Simple Adaptation laws for Upper Bounds on the Norm of the Undcertainties," IEEE Trans. on Automation Control, Vol. 37, No. 6, pp. 860-865, 1992
DOI
ScienceOn
|
13 |
Woo, B., Jung, B., and Chae, J., "Study On the Three-Axes Attitude Controll, Journal of the Korean Society for Aeronautical and Space Sciences, Vol. 25, No. 3, 1997, pp. 148-156
|
14 |
Choi, K., "Fault Tolerant Attitude Estimation Algorithm", Graduate School of Mechanical and Aerospace Engineering in Seoul National University, 2010
|
15 |
B. L. Walcott and S. H. Zak, "Combined observer-controller synthesis for uncertain dynamical systems with applications," IEEE Trans. Syst., Man., Cybern., Vol. 18, No. 1, Feb. 1988, pp. 88-104
DOI
ScienceOn
|
16 |
M. J. Corless and G. Leitmann, "Continuous state feedback guaranteeing uniform ultimate boundedness for uncertain dynamic systems," IEEE Trans. Automat. Contr., Vol. AC-26, No. 5, Oct. 1981, pp. 1139-1143
|
17 |
Azza, EI-S. I., Ahamed, M. T., and Mohammad, A. S., "Satellite Attitude Maneuver Using Sliding Mode Control under Body Angular Velocity Constraints," International Journal of Computer Application, Vol. 50, No. 13, July 2012, pp. 41-46
|
18 |
Lee, H., and Kim, Y., "Fault-tolerant Control Scheme for Satellite Attitude Control System," IET Control Theory Appl., Vol. 4, Iss. 8, 2010, pp. 1436-1450
DOI
ScienceOn
|
19 |
S. A. Kowalchuk, and C. D. Hall, "Spacecraft Attitude Sliding Mode Controller using Reaction Wheels," Proc. of AIAA/AAS Astrodynamics Specialist Conference and Exhibit, Aug. 2008
|
20 |
Son, K., Bae, J., and Kim, Y., "A Study on the Optimal Sliding Mode Control Methods for the Spacecraft Attitude Control," KSAS09-2603, 2009, pp. 655-658
|