Mitigation of angular acceleration effects on optical sensor...

Details Mitigation of angular acceleration effects on optical sensor... Mitigation of angular acceleration effects on optical sensor...

2005-03-08

2005-03-08

Gregory, Bernarr E. (Department: 3662)

Aeronautics and astronautics

Spacecraft

Attitude control

C244S003150, C244S003160, C244S003180, C244S003210, C244S158700, C244S164000, C701S003000, C701S004000, C701S013000, C701S207000, C701S222000

Reexamination Certificate

active

06863244

ABSTRACT:
A method, apparatus, article of manufacture, and a memory structure for compensating for optical sensor data corrupted by angular acceleration is disclosed. The method comprises the steps of determining an angular acceleration of the optical sensor and modifying the optical sensor data according to the determined angular acceleration of the optical sensor. The apparatus comprises a sensor for determining an angular acceleration of the optical sensor and a navigation system for modifying the optical sensor data according to the determined angular acceleration of the optical sensor.

REFERENCES:
patent: 3952151 (1976-04-01), Jenkin
patent: 5660355 (1997-08-01), Waymeyer
patent: 6179246 (2001-01-01), Fisel et al.
patent: 6285927 (2001-09-01), Li et al.
Edward Wong et al., “Post-Flight Attitude Reconstruction for the Shuttle Radar Topography Mission”, American Astronomical Society, AAS 01-314, pp. 213-233, 2001.

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