A computational method for free time optimal control problems, with application to maximizing the range of an aircraft-like projectile

DOI10.1017/S0334270000005476zbMath0654.70031OpenAlexW1967216733MaRDI QIDQ3801141

No author found.

Publication date: 1987

Published in: The Journal of the Australian Mathematical Society. Series B. Applied Mathematics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1017/s0334270000005476

zbMATH Keywords

control parametrization techniquesaircraft-like gliding projectileangle of attack controlnon-standard optimal control problems

Mathematics Subject Classification ID

Free motion of a rigid body (70E15) Control of mechanical systems (70Q05) Existence theories for optimal control problems involving partial differential equations (49J20)

Related Items (4)

The control parameterization method for nonlinear optimal control: a survey ⋮ Optimal control computation for nonlinear systems with state-dependent stopping criteria ⋮ Optimal control problems with stopping constraints ⋮ An exact penalty method for free terminal time optimal control problem with continuous inequality constraints

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