NASA NTRS · 19710061348
Fuel-optimal angular momentum vector control for spinning and dual-spin spacecraft
Abstract
Spinning and dual spin spacecraft angular momentum and axis control, investigating optimal fuel and small angle reorientation techniques
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Larson, V., Likins, P.. 1971-09-01. Fuel-optimal angular momentum vector control for spinning and dual-spin spacecraft. https://ntrs.nasa.gov/citations/19710061348
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