Gradient-Free Trust-Region-Based Adaptive Response Surface Method for Expensive Aircraft Optimization
Author:
Affiliation:
1. Key Laboratory of Dynamics and Control of Flight Vehicle, 100081 Beijing, People’s Republic of China
2. Beijing Institute of Technology, 100081 Beijing, People’s Republic of China
Funder
National Natural Science Foundation of China
Aeronautical Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J054779
Reference30 articles.
1. Review of Metamodeling Techniques in Support of Engineering Design Optimization
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