A Heuristic Approach to Design an Orbit for the Temporary Reconnaissance Mission Using a Few LEO Satellites

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Publisher
American Institute of Aeronautics and Astronautics
Issue Date
2008-01-28
Language
ENG
Citation

2008 AAS/AIAA Space Flight Mechanics Meeting, v.130 PART 2, pp.1393 - 1408

ISSN
0065-3438
URI
http://hdl.handle.net/10203/16535
Appears in Collection
AE-Conference Papers(학술회의논문)

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