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Design of optimal spacecraft‐asteroid formations through a hybrid global optimization approach

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Publication:3526266
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DOI10.1108/17563780810874735zbMath1151.49035OpenAlexW1967198835MaRDI QIDQ3526266

Christie Alisa Maddock, Massimiliano Vasile

Publication date: 25 September 2008

Published in: International Journal of Intelligent Computing and Cybernetics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1108/17563780810874735


zbMATH Keywords

trackingoptimization techniquesspacecraft navigationflight operations


Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90)


Related Items (5)

Multi agent collaborative search based on Tchebycheff decomposition ⋮ Multi Agent Collaborative Search ⋮ A multi-objective approach to the design of low thrust space trajectories using optimal control ⋮ A multi-mirror solution for the deflection of dangerous NEOS ⋮ On the deflection of asteroids with mirrors




Cites Work

  • A hybrid multiagent approach for global trajectory optimization
  • Maximin Latin Hypercube Designs in Two Dimensions




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