Very low-thrust trajectory optimization using a direct SQP method

DOI10.1016/S0377-0427(00)00301-0zbMath0970.65072MaRDI QIDQ1578840

John T. Betts

Publication date: 4 September 2000

Published in: Journal of Computational and Applied Mathematics (Search for Journal in Brave)

zbMATH Keywords

vehicle dynamicssuccessive quadratic programminglow-thrust orbit transfersmission orbitpark orbittrajectory modelingtranscription method

Mathematics Subject Classification ID

Numerical mathematical programming methods (65K05) Applications of mathematical programming (90C90) Transportation, logistics and supply chain management (90B06) Orbital mechanics (70M20) Methods of successive quadratic programming type (90C55)

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Cites Work

• A set modified equinoctial orbit elements
• Path-constrained trajectory optimization using sparse sequential quadratic programming
• On the equinoctial orbit elements
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