Dynamic yaw steering method for spacecrafts

Aeronautics and astronautics – Spacecraft – Attitude control

Reexamination Certificate

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C701S013000

Reexamination Certificate

active

07143982

ABSTRACT:
A method for yaw steering a spacecraft including performing yaw steering of the spacecraft to have a yaw angle (ψ) for all sun elevation angles (β). The method further including smoothing a yaw steering motion for orbital position parameters (η) where high rotational rates {dot over (ψ)} and high rotational accelerations {umlaut over (ψ)} would occur. The instant abstract is neither intended to define the invention disclosed in this specification nor intended to limit the scope of the invention in any way.

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patent: 5791598 (1998-08-01), Rodden et al.
patent: 5794891 (1998-08-01), Polle et al.
patent: 6164597 (2000-12-01), Barker et al.
patent: 6293502 (2001-09-01), Fowell
patent: 6311932 (2001-11-01), Rodden et al.
patent: 6470243 (2002-10-01), Eyerly et al.
patent: 0785132 (1997-07-01), None
patent: 1167189 (2002-01-01), None
L. Barker et al., “Sirius Satellite Design: The Challenges of the Tundra Orbit in Commercial Spacecraft Design”, Guidance and Control 2001, Proceedings of the Annual AAS Rocky Mountain Conference, Jan. 31, 2001, pp. 575-596.
W. Bao, “Materials Quick Reference,” XP—002275236, Jul. 2001, downloaded on Mar. 26, 2004 from URL:http://www.cz3.nus.edu.sg/{bao/teach/cz4206/matqkref.pdf.

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