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Improved Differential Evolution Algorithm and Its Applications to Orbit Design
Abstract
Differential Evolution (DE) is a basic and robust evolutionary strategy that has been applied to determining the global optimum for complex optimization problems[1–5]. It was introduced in 1995 by Storn and Price [1] and has been successfully applied to optimization problems including nonlinear, non-differentiable, non-convex, and multi-model functions. DE algorithms show good convergence, high-reliability, simplicity, and a reduced number of controllable parameters [2]. Olds and Kluever [3] applied DE to an interplanetary trajectory optimization problem and demonstrated the effectiveness of DE to produce rapid solutions. Madavan [4] discussed various modifications to the DE algorithm, improved its computational efficiency, and applied it to aerodynamic shape optimization problems. DE algorithms are easy to use, as they require only a few robust control variables, which can be drawn from a well-defined numerical interval. However, the existing various DE algorithms also have limitations, being susceptible to instability and getting trapped into local optima[2]. Notable effort has been spent addressing this by coupling DE algorithms with other optimization algorithms (for example, Self Organizing Maps (SOM) [6], Dynamic Hill Climbing (DHC) [7], Neural Networks (NN) [7], Particle Swarm Optimization (PSO) [8]). In these cases, the additional algorithm is used as an additional loop within the optimization process, creating a hybrid system with an inner and outer loop. Such hybrid algorithms are inherently more complex and so the computation cost is increased. Attempting to address this, a self-adaptive DE was designed and applied to the orbit design problem for prioritized multiple targets by Chen[5]. However, the self-adaptive feature is somewhat limited as it relates only to the number of generations within the optimization. A Self-adaptive DE which can automatically adapt its learning strategies and the associated parameters during the evolving procedure was proposed by Qin and Suganthan[9] and 25 test functions were used to verify the algorithm.
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“The hybridization of ACO and DE exhibits the effective search capability of DE that has been proved in previous studies [4,26,32].”
From Orbital Maneuver Optimization of Earth Observation Satellites Using an Adaptive Differential Evolution Algorithm (2022) · cites this paper as [26]
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Research works printed but not linked: 10
- 10.1023/A:1008202821328 · DOI · Paper page
- PriceK.StornR. M.LampinenJ. A., Differential Evolution: A Practical Approach to Global Optimization, Springer, New York, 2005, pp. 155–175, 515–520.
- 10.2514/1.27242 · DOI
- 10.2514/6.2004-4622 · DOI
- 10.1061/(ASCE)AS.1943-5525.0000393 · DOI · Paper page
- 10.2514/6.2014-2730 · DOI
- Madavan N. K., 2013, 21st AIAA Applied Aerodynamics Conference
- 10.1016/j.actaastro.2009.05.029 · DOI · Paper page
- CurtisH. D., Orbital Mechanics for Engineering Students, Elsevier Butterworth-Heinemann, Norfolk, U.K., 2005, pp. 616–621.
- ValladoD. A., Fundamentals of Astrodynamics and Applications, Vol. 12, 3rd ed., Springer, New York, Microcosm Press, Hawthorne, CA, 2007, pp. 842–851.
Cited by
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Luo, Q., Peng, W., Wu, G., & Xiao, Y. (2022) · Remote Sensing · doi:10.3390/rs14091966 · Cited by 26
Metadata
- Authors
- Yao, W., Luo, J., Macdonald, M., Wang, M., & Ma, W.
- Affiliations
- Northwestern Polytechnical University (CN)
- University of Strathclyde (GB)
- Venue
- Journal of Guidance, Control, and Dynamics
- Published
- 2018-04
- Volume
- 41
- Issue
- 4
- Pages
- 936-943
- ISSN
- 0731-5090 (ISSN-L)
- 1533-3884
- OpenAlex
- W2767838280
- Cited by
- 14
- References
- 0
- Citations by year
- 2026: 2 · 2025: 2 · 2023: 1 · 2022: 3 · 2020: 2 · 2019: 2 · 2018: 2
- FWCI
- 0.98
- Type
- journal article
- Language
- en
- Open access
- closed
- Locations
- Journal of Guidance Control and Dynamics (publishedVersion)
- Strathprints: The University of Strathclyde institutional repository (University of Strathclyde) (acceptedVersion)
- Funders
- National Natural Scientific Foundation of China (61690210, 61690211)
- Topics
- Physical Sciences › Computer Science › Artificial Intelligence › Metaheuristic Optimization Algorithms Research
- Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Dynamics and Control
- Physical Sciences › Engineering › Aerospace Engineering › Space Satellite Systems and Control
- Keywords
- differential evolution, self-adaptive differential evolution, orbit design, interplanetary trajectory optimization, hybrid evolutionary algorithm, local optima avoidance, parameter adaptation
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- CoChat. (2026). Citation check: Improved Differential Evolution Algorithm and Its Applications to Orbit Design. https://app.cochat.ai/papers/10.2514/1.g003214
- The paper
- Yao, W., Luo, J., Macdonald, M., Wang, M., & Ma, W. (2018). Improved Differential Evolution Algorithm and Its Applications to Orbit Design. Journal of Guidance, Control, and Dynamics. https://doi.org/10.2514/1.g003214