Minimum Time Control of the Rocket Attitude Reorientation Associated with Orbit Dynamics

DOI10.1137/15M1028716zbMath1338.49046arXiv1507.00172OpenAlexW2242835355MaRDI QIDQ2796010

Max Cerf, Jia-Min Zhu, Emmanuel Trélat

Publication date: 23 March 2016

Published in: SIAM Journal on Control and Optimization (Search for Journal in Brave)

Full work available at URL: https://arxiv.org/abs/1507.00172

zbMATH Keywords

optimal controlcontinuationshooting methodPontryagin maximum principlechattering arcscoupled attitude orbit problem

Mathematics Subject Classification ID

Numerical mathematical programming methods (65K05) Nonlinear programming (90C30) Numerical optimization and variational techniques (65K10) Numerical methods based on necessary conditions (49M05) Applications of optimal control and differential games (49N90) Numerical methods based on nonlinear programming (49M37) Variable mass, rockets (70P05) Global methods, including homotopy approaches to the numerical solution of nonlinear equations (65H20) Optimality conditions for problems involving ordinary differential equations (49K15)

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Uses Software

• HYBRJ
• minpack
• SOCS
• Bocop

Cites Work

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