Multidisciplinary design and optimization of an air launched satellite launch vehicle using a hybrid heuristic search algorithm

Engineering Optimization

Volumn 43, Issue 3, 2011, Pages 305-328

  Rafique, A F ^a   He, L S ^a   Zeeshan, Q ^a   Kamran, A ^a   Nisar, K ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

genetic algorithm; hybrid heuristic search algorithm; multidisciplinary design optimization; satellite launch vehicle; simulated annealing

Indexed keywords

DESIGN OBJECTIVES; DESIGN SPACES; DESIGN STRATEGIES; FEASIBLE REGIONS; HIGH FIDELITY MODELS; HYBRID HEURISTIC SEARCH ALGORITHM; HYBRID HEURISTICS; LOW EARTH ORBITS; MASS PROPERTIES; MULTI-DISCIPLINARY DESIGNS; MULTIDISCIPLINARY DESIGN AND OPTIMIZATION; MULTIDISCIPLINARY DESIGN OPTIMIZATION; OPTIMAL SOLUTIONS; OPTIMALITY; PERFORMANCE CONSTRAINTS; SATELLITE LAUNCH VEHICLE; SATELLITE LAUNCH VEHICLES; SOLID PROPULSION;

COMBINATORIAL OPTIMIZATION; DESIGN; FLIGHT DYNAMICS; GENETIC ALGORITHMS; LAUNCH VEHICLES; LAUNCHING; LEARNING ALGORITHMS; MODULAR ROBOTS; SATELLITES; SPACECRAFT PROPULSION; VEHICLES;

SIMULATED ANNEALING;

EID: 79951546285     PISSN: 0305215X     EISSN: 10290273     Source Type: Journal    
DOI: 10.1080/0305215X.2010.489608     Document Type: Article

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