Closed-Form Solutions for Minimum-Time Paths of Dubins Airplane in Steady Wind
Fanchen Wu (1), Zheng Chen (1, 2) ((1) School of Aeronautics and, Astronautics, Zhejiang University, Hangzhou, China, (2) Huanjiang Laboratory,, Zhuji, China)

TL;DR
This paper derives closed-form solutions for the minimum-time paths of a Dubins airplane affected by steady wind, enabling rapid computation of globally optimal routes through geometric analysis and an improved root-finding method.
Contribution
It introduces a novel closed-form solution framework for minimum-time Dubins airplane paths under steady wind, including an efficient root-finding algorithm for nonlinear equations.
Findings
Closed-form solutions for all path types are derived.
The proposed method computes the globally optimal path in constant time.
Numerical examples confirm the effectiveness and optimality of the solutions.
Abstract
This paper is concerned with the minimum-time path-planning problem for a Dubins airplane under the influence of steady wind. The path-planning problem, by transforming into the air-relative frame, is equivalent to finding the minimum-time control strategy for a Dubins airplane to intercept a moving target. In the air-relative frame, by applying Pontryagin's maximum principle, the candidates for the minimum-time solution are categorized into a family of four types: SC, CC, CCC, CSC, where S denotes a straight line segment and C denotes a circular segment. Furthermore, the geometric properties for each type are analyzed, indicating that the paths of SC and CC can be obtained by finding the roots of a quadratic equation, while the paths of CCC and CSC are determined by the roots of some nonlinear transcendental equations. An improved bisection method is presented in the paper so that all…
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Taxonomy
TopicsAerospace Engineering and Control Systems · Robotic Path Planning Algorithms · Spacecraft Dynamics and Control
