Trajectory optimization for maneuvering satellites

DOI10.1016/0167-6911(85)90013-1zbMath0554.49019OpenAlexW2030742588MaRDI QIDQ759998

Bruce R. Feiring, Ken Tomita

Publication date: 1985

Published in: Systems \& Control Letters (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0167-6911(85)90013-1

zbMATH Keywords

optimal trajectoriesexact penalty function methodmaneuvering satellite

Mathematics Subject Classification ID

Numerical optimization and variational techniques (65K10) Numerical methods based on nonlinear programming (49M37) Orbital mechanics (70M20) Control/observation systems governed by ordinary differential equations (93C15) Optimality conditions for problems involving ordinary differential equations (49K15)

Cites Work

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• An exact penalty method for solving optimal control problems
• A Steepest-Ascent Method for Solving Optimum Programming Problems
• Solution of variational problems by means of a generalized newton-raphson operator
• Optimization and Control of Nonlinear Systems Using the Second Variation

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