Title :
Integral guidance for ballistic missiles
Author_Institution :
Computer Sciences Corporation, Huntsville, Alabama
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;
Conference_Titel :
Decision and Control including the 15th Symposium on Adaptive Processes, 1976 IEEE Conference on
Conference_Location :
Clearwater, FL, USA
DOI :
10.1109/CDC.1976.267661
