NASA NTRS · 19880000207
Determining Spacecraft Attitude For Planetary Mapping
Abstract
New algorithm calculates attitude with accuracy to spare. Report describes algorithm for use in determining attitude of spacecraft from incremental-angle output of strapdown gyroscope and star-scanner measurements. Highlights detail of underlying theories and strategies. Presents results of simulation to demonstrate capability of algorithm, and discusses possible applications.
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Huang, Whitak H., Reddy, Narotham S.. 1988-03-01. Determining Spacecraft Attitude For Planetary Mapping. https://ntrs.nasa.gov/citations/19880000207
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