| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 5028773 | Procedia Engineering | 2017 | 8 Pages |
Abstract
A small information satellite which may be placed on an orbit with altitude from 600 up to 1000Â km is considered. The satellite attitude and orbit control system contains a strap-down inertial navigation system, cluster of four reaction wheels, magnetic driver and a correcting engine unit with eight electro-reaction engines. Problems on the design of algorithms for control of the satellite spatial motion on sun-synchronous orbit are studied.
Related Topics
Physical Sciences and Engineering
Engineering
Engineering (General)
Authors
Yevgeny Somov, Olga Starinova, Sergey Butyrin,