The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Nov. 18, 1997

Filed:

Oct. 16, 1995
Applicant:
Inventors:

Neil Evan Goodzeit, Princeton, NJ (US);

Santosh Ratan, Lawrenceville, NJ (US);

Assignee:

Martin Marietta Corporation, East Windsor, NJ (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64G / ; B64G / ;
U.S. Cl.
CPC ...
244169 ; 244171 ; 244172 ; 244173 ;
Abstract

A spacecraft includes a three-axis attitude control system. When velocity change thrusters are fired, their plumes impinge on a solar array, at angles which vary with the solar array position. This causes disturbance torques which vary with the solar array position. Disturbance torque information signals or torque bias signals which depend upon the solar array angle are summed with the torque demand signals which control the attitude control system during firing of the velocity change thrusters, to modify the attitude correction torques. The bias torque signals are generated by a Fourier processor based upon stored Fourier coefficients together with signals from a solar array angular position sensor.


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