DocumentCode :
3496972
Title :
Optimal guidance for missiles with varying velocity
Author :
Cho, Hangju ; Chang Kyung Ryoo ; Tahk, Min-Jea
Author_Institution :
Agency for Defense Dev., Taejeon, South Korea
fYear :
1995
fDate :
26-28 Jul 1995
Firstpage :
1503
Lastpage :
1508
Abstract :
An optimal guidance law for missiles with time-varying velocity is investigated. The closed-form solution is derived and properties of the key variables of the solution such as a tgo-like function and the time-varying guidance gain are studied. Simulation studies show an excellent performance of the proposed guidance law
Keywords :
missile guidance; optimal control; time-varying systems; closed-form solution; missiles; optimal guidance law; tgo-like function; time-varying guidance gain; time-varying velocity; Art; Cathode ray tubes; Closed-form solution; Equations; Geometry; Gold; Missiles; Optimal control; Virtual manufacturing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
SICE '95. Proceedings of the 34th SICE Annual Conference. International Session Papers
Conference_Location :
Hokkaido
Print_ISBN :
0-7803-2781-0
Type :
conf
DOI :
10.1109/SICE.1995.526737
Filename :
526737
Link To Document :
https://search.ricest.ac.ir/dl/search/defaultta.aspx?DTC=49&DC=3496972
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