Improved Differential Evolution Algorithm and Its Applications to Orbit Design-Reference-Cited by-同舟云学术

Improved Differential Evolution Algorithm and Its Applications to Orbit Design

Published:2018-04 Issue:4 Volume:41 Page:936-943
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Yao Wei,Luo Jianjun,Macdonald Malcolm¹,Wang Mingming,Ma Weihua

Affiliation:

1. University of Strathclyde, Glasgow, Scotland G1 1XJ, United Kingdom

Funder

National Natural Scientific Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.G003214

Reference11 articles.

1. PriceK.StornR. M.LampinenJ. A., Differential Evolution: A Practical Approach to Global Optimization, Springer, New York, 2005, pp. 155–175, 515–520.

2. Interplanetary Mission Design Using Differential Evolution

3. On Improving Efficiency of Differential Evolution for Aerodynamic Shape Optimization Applications

4. Optimal Satellite Orbit Design for Prioritized Multiple Targets with Threshold Observation Time Using Self-Adaptive Differential Evolution

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