DocumentCode
3015819
Title
Integral guidance for ballistic missiles
Author
Bishop, C.M.
Author_Institution
Computer Sciences Corporation, Huntsville, Alabama
fYear
1976
fDate
1-3 Dec. 1976
Firstpage
1159
Lastpage
1163
Abstract
An integral guidance technique is proposed which uses the line-of-sight angle, as well as line-of-sight rate to determine the guidance command. Integral guidance is compared with proportional navigation guidance in a ballistic missile application and is found to reduce trajectory dispersions caused by disturbances.
Keywords
Application software; Computer vision; Control systems; Differential equations; Drives; Integral equations; Missiles; Navigation; Turning; Virtual manufacturing;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control including the 15th Symposium on Adaptive Processes, 1976 IEEE Conference on
Conference_Location
Clearwater, FL, USA
Type
conf
DOI
10.1109/CDC.1976.267661
Filename
4045769
Link To Document