Slew Control of Prolate Spinners Using Single Magnetorquer

E XISTING research [1–5] on the prolate spinning spacecraft attitude maneuver has developed a series of slew algorithms using a single thruster in two categories: half-cone derived algorithms and pulse-train algorithms. Half-cone derived algorithms consist of half-cone (HC), multi-half-cone, dual-...

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Bibliographic Details
Main Authors: Juntian, Si, Yang, Gao, Abadi, Chanik
Format: Article
Language:English
Published: American Institute of Aeronautics and Astronautics 2016
Subjects:
Online Access:http://ir.unimas.my/id/eprint/39136/5/Slew%20Control%20-%20Copy.pdf
http://ir.unimas.my/id/eprint/39136/
https://arc.aiaa.org/journal/jgcd
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Institution: Universiti Malaysia Sarawak
Language: English
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