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NASA NTRS ยท 19840009181

Development of an autonomous video rendezvous and docking system, phase 3

Abstract

Field-of-view limitations proved troublesome. Higher resolution was required. Side thrusters were too weak. The strategy logic was improved and the Kalman filter was augmented to estimate target attitude and tumble rate. Two separate filters were used. The new filter estimates target attitude and angular momentum. The Newton-Raphson iteration improves image interpretation.

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BibTeXRIS

Tietz, J. C.. 1984-01-01. Development of an autonomous video rendezvous and docking system, phase 3. https://ntrs.nasa.gov/citations/19840009181

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