Aeronautics and astronautics – Spacecraft – Attitude control
Patent
1991-07-17
1993-03-16
Barefoot, Galen
Aeronautics and astronautics
Spacecraft
Attitude control
244164, B64G 124
Patent
active
051937662
ABSTRACT:
In a rendezvous maneuver for approaching a rendezvous spacecraft to a target spacecraft through a reference trajectory for approach which is different in altitude and period from a trajectory of the target spacecraft, when the rendezvous spacecraft is deviated from the reference trajectory for approach as a result from a failure in the maneuver, it is first maneuvered in the direction of altitude after 0.2 revolutions of the rendezvous spacecraft, and then maneuvered in the direction of phase after another 0.2 revolutions. The rendezvous spacecraft is thereby restored to the reference trajectory with no fear of entering a collision course, so that high reliable retry/recovery may be performed promptly and safely.
REFERENCES:
patent: 4898349 (1990-02-01), Miller
Kaplan, Modern Spacecraft Dynamics and Control, John Wiley & Sons (pbl), 1976, pp. 108-115.
Kawano Isao
Nakamura Hiroyuki
Suzuki Takahiro
Wakabayashi Yasufumi
Barefoot Galen
National Space Development Agency of Japan
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