Design of a guided missile interceptor using a genetic algorithm

Journal of Spacecraft and Rockets

Volumn 38, Issue 1, 2001, Pages 28-35

  Anderson, M B ^b   Burkhalter, J E ^a   Jenkins, R M ^a  

^a AUBURN UNIVERSITY   (United States)

^b NONE

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMBUSTION CHAMBERS; COMPUTER AIDED DESIGN; ELECTRONIC GUIDANCE SYSTEMS; GENETIC ALGORITHMS; OPTIMIZATION; PARETO PRINCIPLE; TRAJECTORIES;

FUEL VOLUME RATIO; GUIDED MISSILE INTERCEPTOR;

MISSILES;

EID: 0035081636     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.3668     Document Type: Article

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