Evolutionary algorithm applied to ballistic launch vehicle design using hybrid rocket engine evaluated by enhanced flight simulation.
Hideyuki YodaShoma ItoMasahiro KanazakiKazuhisa ChibaKoki KitagawaToru ShimadaPublished in: CEC (2015)
Keyphrases
- evolutionary algorithm
- flight control
- optimization problems
- case study
- user interface
- real time
- life cycle
- simulation environment
- multidisciplinary design optimization
- autonomous underwater vehicle
- fuel consumption
- molecular dynamics
- air traffic control
- computer aided design
- hybrid learning
- engineering design
- design process