Control and trajectory optimization of an aircraft's alignment with the desired track

DOI10.1134/S1064230717040165zbMath1387.49029OpenAlexW2764307906MaRDI QIDQ1745887

A. A. Golubeva, Yu. O. Volodina, N. V. Kulanov

Publication date: 18 April 2018

Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s1064230717040165

zbMATH Keywords

maximum principlealigning an aircraftoptimal trajectory lengthsynthesis of the control

Mathematics Subject Classification ID

Synthesis problems (93B50) Control problems involving ordinary differential equations (34H05) Optimality conditions for problems involving ordinary differential equations (49K15)

Cites Work

• Kinematic algorithms for controlling aircraft during flight toward a target and while turning to a new heading
• Three-dimensional reachability set for a nonlinear control system
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