Kelly et al., 1994 - Google Patents
Stationkeeping of geostationary satellites with simultaneous eccentricity and longitude controlKelly et al., 1994
- Document ID
- 9586157299413503896
- Author
- Kelly T
- White L
- Gamble D
- Publication year
- Publication venue
- Journal of Guidance, Control, and Dynamics
External Links
Snippet
METHODS of orbital control of geostationary satellites is of continuing interest due to stringent constraints imposed upon the satellite motion by ground-based antennas. The two traditional aspects of orbital control are referred to as north/south (N/S, which controls …
- 230000000694 effects 0 abstract description 29
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- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
- B64G1/283—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
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- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
- B64G1/281—Spin-stabilised spacecraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B64G1/32—Guiding or controlling apparatus, e.g. for attitude control using earth's magnetic field
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