DocumentCode
1462582
Title
Inertial systems in space vehicles
Author
Matthews, M.A.V.
Volume
22
Issue
3
fYear
1961
fDate
9/1/1961 12:00:00 AM
Firstpage
231
Lastpage
239
Abstract
This paper discusses the use of inertial elements in space vehicles for attitude control and navigation. Some limitations of inertial systems in this environment are described and it is shown that inertia alone is not adequate for most space applications. However, the use of inertia to bridge the gaps between information from other sources can simplify the requirements for other sensors in the satellite, and also on the ground tracking equipment. This is illustrated by some examples and by discussion of space vehicle.
Keywords
artificial satellites;
fLanguage
English
Journal_Title
Radio Engineers, Journal of the British Institution of
Publisher
iet
Type
jour
DOI
10.1049/jbire.1961.0111
Filename
5259653
Link To Document