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System and method for correcting attitude estimationA system includes an angular rate sensor disposed in a vehicle for providing angular rates of the vehicle, and an instrument disposed in the vehicle for providing line-of-sight control with respect to a line-of-sight reference. The instrument includes an integrator which is configured to integrate the angular rates of the vehicle to form non-compensated attitudes. Also included is a compensator coupled across the integrator, in a feed-forward loop, for receiving the angular rates of the vehicle and outputting compensated angular rates of the vehicle. A summer combines the non-compensated attitudes and the compensated angular rates of the to vehicle to form estimated vehicle attitudes for controlling the instrument with respect to the line-of-sight reference. The compensator is configured to provide error compensation to the instrument free-of any feedback loop that uses an error signal. The compensator may include a transfer function providing a fixed gain to the received angular rates of the vehicle. The compensator may, alternatively, include a is transfer function providing a variable gain as a function of frequency to operate on the received angular rates of the vehicle.
Document ID
20100028310
Acquisition Source
Goddard Space Flight Center
Document Type
Other - Patent
Authors
Josselson, Robert H.
Date Acquired
August 24, 2013
Publication Date
June 1, 2010
Subject Category
Communications And Radar
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-11/337,889
Patent Number: US-Patent-7,729,816
Funding Number(s)
CONTRACT_GRANT: NNG04HZ07C
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-7,729,816
Patent Application
US-Patent-Appl-SN-11/337,889
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