Orbital Maneuver using Two-Step Sliding Mode Control
The solutions of orbital maneuver problem using the sliding mode control in the presence of the earth gravitational perturbations is obtained. Especially, the optimization of consuming fuel for maneuver is performed. The impulsive solution to Lambert's problem using the combined equation method...
Main Authors: | , , |
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Format: | Article |
Language: | English |
Published: |
The Korean Space Science Society
1998-06-01
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Series: | Journal of Astronomy and Space Sciences |
Online Access: | http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/1998/v15n1/OJOOBS_1998_v15n1_235.pdf |