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-...

Full description

Saved in:
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
Tags: Add Tag
No Tags, Be the first to tag this record!