Title:
エネルギー効率に優れた衛星の操縦
Document Type and Number:
Japanese Patent JP6989252
Kind Code:
B2
Abstract:
Energy efficient satellite maneuvering is described herein. One disclosed example method includes maneuvering a satellite that is in an orbit around a space body so that a principle sensitive axis of the satellite is oriented to an orbit frame plane to reduce gravity gradient torques acting upon the satellite. The orbit frame plane is based on an orbit frame vector.
Inventors:
Louis, Timothy S.
Lee, Kansik
Lee, Kansik
Application Number:
JP2016217175A
Publication Date:
January 05, 2022
Filing Date:
November 07, 2016
Export Citation:
Assignee:
The Boeing Company
International Classes:
B64G1/10; B64G1/24; B64G1/26; B64G1/28
Domestic Patent References:
| JP2004210032A | ||||
| JP200237200A | ||||
| JP2010533290A | ||||
| JP2017511885A |
Foreign References:
| US20080128559 | ||||
| CN104038272A |
Other References:
Bryce A. Roberts, Jeffrey W. Kruk, Thomas B. Ake, Tom S. Englar, Brian F. Class and Daniel M. Rovner,“Three-axis Attitude Control with Two Reaction Wheels and Magnetic Torquer Bars”,AIAA Guidance, Navigation, and Control Conference and Exhibit 16-19 August 2004, Providence, Rhode Island, [online],米国,American Institute of Aeronautics and Astronautics,2012年06月22日,p. 1-8,https://archive.stsci.edu/fuse/papers/mp/AIAA_2004.pdf,[令和2年7月10日検索], インターネット
Attorney, Agent or Firm:
Sonoda/Kobayashi Patent Business Corporation