Time-optimal of fixed wing UAV aircraft with input and output constraints

DOI10.3934/NACO.2021023zbMath1493.49002OpenAlexW3182260239MaRDI QIDQ2167958

M. H. Shavakh, Behroz Bidabad

Publication date: 1 September 2022

Published in: Numerical Algebra, Control and Optimization (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.3934/naco.2021023

zbMATH Keywords

optimizationtime-optimal controlexact penalty functionUAV airplane

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Numerical methods based on nonlinear programming (49M37) Existence theories for optimal control problems involving ordinary differential equations (49J15)

Cites Work

• Unnamed Item
• On the smoothing of the square-root exact penalty function for inequality constrained optimization
• Global stabilization and restricted tracking for multiple integrators with bounded controls
• Shortest paths of bounded curvature in the plane
• A truck and drones model for last-mile delivery: a mathematical model and heuristic approach
• Real-time path planning with limited information for autonomous unmanned air vehicles
• Optimal control problems with multiple characteristic time points in the objective and constraints
• On Curves of Minimal Length with a Constraint on Average Curvature, and with Prescribed Initial and Terminal Positions and Tangents
• A Complete Approximation Algorithm for Shortest Bounded-Curvature Paths
• An Application of the Maximum Principle to the Geometry of Plane Curves
• Projected Sequential Quadratic Programming Methods

This page was built for publication: Time-optimal of fixed wing UAV aircraft with input and output constraints