Title:
宇宙船の動きを制御するシステム及び方法
Document Type and Number:
Japanese Patent JP5901504
Kind Code:
B2
Abstract:
A motion of an object is controlled from a geostationary transit orbit (GTO) of an earth to an orbit of a moon. A first trajectory of the motion of the object is determined from an intermediate orbit of an earth to a neighborhood of a stable manifold of a first Lagrange point (L1). A second trajectory of the motion of the object is determined from the GTO to the intermediate orbit. A third trajectory of the motion of the object is determined from the neighborhood to the stable manifold to an L1 orbit, and a fourth trajectory of the motion of the object is determined from the L1 orbit to the orbit of the moon. A trajectory from the GTO to the orbit of the moon is determined based on a combination of the first, the second, the third, and the fourth trajectories.
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Inventors:
Piyush Glover
Christian Anderson
Christian Anderson
Application Number:
JP2012267985A
Publication Date:
April 13, 2016
Filing Date:
December 07, 2012
Export Citation:
Assignee:
Mitsubishi Electric Corporation
International Classes:
B64G1/10
Domestic Patent References:
| JP2005088891A |
Foreign References:
| US5507454 | ||||
| US5158249 | ||||
| US6385512 |
Attorney, Agent or Firm:
Michiharu Soga
Suzuki Kenchi
Kajinami order
Kazuhiro Oyaku
Shunichi Ueda
Junichiro Yoshida
Satoshi Iino
Suzuki Kenchi
Kajinami order
Kazuhiro Oyaku
Shunichi Ueda
Junichiro Yoshida
Satoshi Iino