Simplified onboard attitude control based on star sensing

Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – Aeronautical vehicle

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Details

701222, 244171, 2502036, G05D 100

Patent

active

060120002

ABSTRACT:
An onboard star tracking system is used to provide continuous attitude data based on a fixed star catalog. An orbital position reference for the sensed star data is estimated from uploaded data. The attitude is calculated based solely on the star sensor data referenced to the estimated orbital position and compared to mission attitude to generate an attitude adjustment.

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patent: 5177686 (1993-01-01), Boinghoff et al.
patent: 5745869 (1998-04-01), van Bezooijen
Liebe, Star Trackers for Attitude Determination, IEEE Aerospace and Elec. Sys. Magazine, vol. 10, Iss. 6, pp. 10-16, Jun. 1996.
Baldini et al., Star-Configuration Searching for Satellite Attitude Computation, IEEE Aerospace and Elec. Sys., vol. 31, Iss. 2, pp. 768-777, Apr. 1995.
Eisenman et al., Real Sky Performance of the Prototype Orsted Advanced Stellar Compass, IEEE Aerospace Applications Conference, Feb. 1996, vol. 2, pp. 103-113.

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