Design of an air to air interceptor using genetic algorithms

1999 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1999, Pages 772-780

  Anderson, Murray B ^a   Burkhalter, John E ^b   Jenkins, Rhonald M ^b  

^a JACOBS TECHNOLOGY   (United States)

^b AUBURN UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ALGORITHMS; COMBUSTION CHAMBERS; FUELS; GENETIC ALGORITHMS; OPTIMIZATION; ROCKET ENGINES; ROCKETS;

AERODYNAMIC DESIGNS; AIR INTERCEPTOR; DESIGN VARIABLES; OPTIMIZATION PROBLEMS; PARETO GENETIC ALGORITHMS; PRELIMINARY DESIGN; SOLID ROCKET MOTORS; THREE-LOOP AUTOPILOT;

DESIGN;

EID: 84959163022     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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15. Anderson, M. B., "Design of a Missile Interceptor Using Genetic Algorithms", Dissertation, Auburn University, Auburn, Alabama, 1998.