Pulse-width Control of Electro-reaction Engines for a Station-keeping of Land-survey Satellite on Sun-synchronous Orbit

A small information satellite which may be placed on an orbit with altitude from 600 up to 1000km 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...

Full description

Saved in:
Bibliographic Details
Published in:Procedia engineering 2017, Vol.185, p.267-274
Main Authors: Somov, Yevgeny, Starinova, Olga, Butyrin, Sergey
Format: Article
Language:English
Subjects:
attitude and orbit control
electro-reaction engines
small satellite
station-keeping
sun-synchronous orbit
Citations: Items that this one cites
Items that cite this one
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
Description
Summary:A small information satellite which may be placed on an orbit with altitude from 600 up to 1000km 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.
ISSN:1877-7058
1877-7058
DOI:10.1016/j.proeng.2017.03.340