Genetic Algorithm Applied to the Time-Series Landing Flight Path and Control Optimization of a Supersonic Transport
Author:
Affiliation:
1. Tokyo Metropolitan University, Tokyo, Japan
Publisher
ACM
Link
https://dl.acm.org/doi/pdf/10.1145/3325773.3325789
Reference13 articles.
1. {DATCOM 1978} 1978. R. D. Fink. 2002. USAF Stability and Control DATCOM Flight Control Division. AFWALTR-83-3048 (1978). {DATCOM 1978} 1978. R. D. Fink. 2002. USAF Stability and Control DATCOM Flight Control Division. AFWALTR-83-3048 (1978).
2. A fast and elitist multiobjective genetic algorithm: NSGA-II
3. } L. E. Ericsson. 1996. Pitch rate effects on delta wing vortex breakdown;Ericsson;J. Aircraft,1996
4. {Eshelman and Schaffer 1993} L.J. Eshelman and J.D. Schaffer. 1993. Real-Coded Genetic Algorithms and Interval-Schemata. Foundations of Genetic Algorithms2 187--202. {Eshelman and Schaffer 1993} L.J. Eshelman and J.D. Schaffer. 1993. Real-Coded Genetic Algorithms and Interval-Schemata. Foundations of Genetic Algorithms2 187--202.
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