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A method of determining attitude from magnetometer data only

Author
Natanson, G. A.
Published
Dec 1, 1990.
Physical Description
1 electronic document
Additional Creators
Nicklas, R. C. and Mclaughlin, S. F.
Online Version

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Unclassified, Unlimited, Publicly available.
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Summary
Presented here is a new algorithm to determine attitude using only magnetometer data under the following conditions: (1) internal torques are known and (2) external torques are negligible. Torque-free rotation of a spacecraft in thruster firing acquisition phase and its magnetic despin in the B-dot mode give typical examples of such situations. A simple analytical formula has been derived in the limiting case of a spacecraft rotating with constant angular velocity. The formula has been tested using low-frequency telemetry data for the Earth Radiation Budget Satellite (ERBS) under normal conditions. Observed small oscillation of body-fixed components of the angular velocity vector near their mean values result in relatively minor errors of approximately 5 degrees. More significant errors come from processing digital magnetometer data. Higher resolution of digitized magnetometer measurements would significantly improve the accuracy of this deterministic scheme. Tests of the general version of the developed algorithm for a free-rotating spacecraft and for the B-dot mode are in progress.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19910007781.
Accession ID: 91N17094.
NASA, Goddard Space Flight Center, Flight Mechanics(Estimation Theory Symposium, 1990; p 359-378.
Terms of Use and Reproduction
No Copyright.
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