DocumentCode
817053
Title
Control, navigation, and guidance
Author
Draper, Charles Stark
Author_Institution
The Charles Stark Draper Laboratory, Inc., Cambridge, MA, USA
Volume
1
Issue
4
fYear
1981
fDate
12/1/1981 12:00:00 AM
Firstpage
4
Lastpage
17
Abstract
Self-contained systems providing control and navigation for vehicles of all kinds use gyroscopic elements to maintain reference directions with respect to inertial space. Sensors for resultant gravity field and inertial reaction forces along input axes determine the vertical and also linear velocities with respect to inertial space. These components divided by an equivalent Earth radius transfer the motion to Earth coordinates in which integration gives location. Corrections for Earth´s rotation projected in and perpendicular to the horizontal plane are made as computed cosine and sine projections of Earth´s angular velocity. Current systems result with the order of fractional miles per hour performance.
Keywords
Aircraft control; Inertial navigation; Gyroscopes; Navigation; Sensors; Velocity control;
fLanguage
English
Journal_Title
Control Systems Magazine, IEEE
Publisher
ieee
ISSN
0272-1708
Type
jour
DOI
10.1109/MCS.1981.1100795
Filename
1100795
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