Time Optimal Attitude Maneuver Strategies for the Agile Spacecraft with Reaction Wheels and Thrusters
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Lee Byung-Hoon
(School of Aerospace and Mechanical Engineering, Hankuk Aviation University)
Lee Bong-Un (School of Aerospace and Mechanical Engineering, Hankuk Aviation University) Oh Hwa-Suk (School of Aerospace and Medhanical Engineering, Hankuk Aviation University) Lee Seon-Ho (Group of Satellite Control System, Korea Aerospace Research Institute) Rhee Seung-Wu (Group of Satellite Control System, Korea Aerospace Research Institute) |
1 | Sidi, M., 1997, Spacecraft Dynamics and Control, Cambridge University Press, pp. 287-289 |
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7 | Oh, H. S., Kwon, J. W., Lee, H., Nam, M. R. and Park, D. J., 2001, 'Torque and Force Measurement of a Prototype HAU Reaction Wheel and the Effect of Disturbance on the Attitude Stability of spacecraft,' KSME International Journal, Vol. 15, No. 6, pp. 743-751 과학기술학회마을 |
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9 | Oh, H. S. and Hwang, J. H., 1999, 'Minimum Fuel Back-Up Attitude Control and Momentum Dumping of a Satellite with an Asymmetric Thruster Configuration,' Journal of Korean Society for Aeronautical and Space Sciences in Korea, Vol. 27, No. 6, pp. 105-115 |
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12 | KARI and HAU, 2003, 'Varying Time Division Pulsing Method and its Controller for Coupled Thrusting Satellite,' Patent Pending in Korea |
13 | Lee, B. H., 2004, 'Time Optimal Attitude Maneuvers for Agile Spacecraft with Thrusters and Reaction Wheels,' Thesis, M.S., Department of Aerospace and Mechanical Engineering, Hankuk Aviation University, Korea |
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