Trajectory optimization of space vehicle in rendezvous proximity operation with evolutionary feasibility conserving techniques-Reference-Cited by-同舟云学术

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Trajectory optimization of space vehicle in rendezvous proximity operation with evolutionary feasibility conserving techniques

Published:2023-01 Issue: Volume:117 Page:105523
ISSN:0952-1976
Container-title:Engineering Applications of Artificial Intelligence
language:en
Short-container-title:Engineering Applications of Artificial Intelligence

Author:

Shirazi Abolfazl^ORCID,Ceberio Josu^ORCID,Lozano Jose A.

Publisher

Elsevier BV

Subject

Electrical and Electronic Engineering,Artificial Intelligence,Control and Systems Engineering

Reference34 articles.

1. Spacecraft Formation Flying: Dynamics, Control and Navigation, Vol. 2;Alfriend,2009

2. Mapped adjoint control transformation method for low-thrust trajectory design;Ayyanathan;Acta Astronaut.,2022

3. The not-a-knot piecewise interpolatory cubic polynomial;Behforooz;Appl. Math. Comput.,1992

4. Unified multiobjective optimization scheme for aeroassisted vehicle trajectory planning;Chai;J. Guid. Control Dyn.,2018

5. Solving constrained trajectory planning problems using biased particle swarm optimization;Chai;IEEE Trans. Aerosp. Electron. Syst.,2021

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. AI and Robots Impact on Space Exploration;Advances in Astronautics Science and Technology;2024-02-01

2. A knowledge-driven co-evolutionary algorithm assisted by cross-regional interactive learning;Engineering Applications of Artificial Intelligence;2023-11

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