Minimum-time three-dimensional turn to a point of supersonic aircraft

DOI10.2514/3.19783zbMath0496.49012OpenAlexW2055342720MaRDI QIDQ3961390

Ching-Fang Lin

Publication date: 1982

Published in: Journal of Guidance, Control, and Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.19783

zbMATH Keywords

maximum principleoptimal switchingoptimal trajectorysupersonic aircraftminimum- time turnoptimal aerodynamic controloptimal thrust controlsingular thrust control

Mathematics Subject Classification ID

Numerical methods based on necessary conditions (49M05) Hamilton-Jacobi equations in mechanics (70H20) Control/observation systems governed by ordinary differential equations (93C15) Optimality conditions for problems involving ordinary differential equations (49K15)

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