Optimal Trajectory Correction Maneuver Design Using the B-Plane Targeting Method for Future Korean Mars Missions
Optimal Trajectory Correction Maneuver (TCM) design algorithm has been developed using the B-plane targeting method for future Korean Mars missions. For every mission phase, trajectory informations can also be obtained using this developed algorithms which are essential to design optimal TCM strateg...
Main Authors: | , , , , , , , , |
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Format: | Article |
Language: | English |
Published: |
Korean Space Science Society (KSSS)
2005-12-01
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Series: | Journal of Astronomy and Space Sciences |
Subjects: | |
Online Access: | http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2005/v22n4/OJOOBS_2005_v22n4_451.pdf |