Title
Real-Time Optimized Trajectory Planning For A Fixed-Wing Vehicle Flying In A Dynamic Environment
Keywords
Aircraft; Collision; Control; Motion; Optimization
Abstract
The problem of determining an optimal feasible trajectory, for a fixed wing flying vehicle moving in a dynamical three-dimensional space, is addressed in this paper, and an analytical solution is proposed. With explicitly considering the boundary conditions and kinematic constraints as well as by satisfying the collision avoidance criterions, trajectories are described in terms of three parameterized polynomials, and the family of feasible trajectories are found. Then, the desired near shortest trajectory is chosen from the feasible trajectories by optimizing a performance index with respect to L2 norm. This trajectory and its associated steering controls are achieved analytically. Computer simulations validate that this approach is computationally efficient and real-time implementable. © 2009 ASCE.
Publication Date
9-28-2009
Publication Title
Journal of Aerospace Engineering
Volume
22
Issue
4
Number of Pages
331-341
Document Type
Article
Personal Identifier
scopus
DOI Link
https://doi.org/10.1061/(ASCE)0893-1321(2009)22:4(331)
Copyright Status
Unknown
Socpus ID
70349310419 (Scopus)
Source API URL
https://api.elsevier.com/content/abstract/scopus_id/70349310419
STARS Citation
Yang, Jian; Qu, Zhihua; Wang, Jing; and Hull, Richard A., "Real-Time Optimized Trajectory Planning For A Fixed-Wing Vehicle Flying In A Dynamic Environment" (2009). Scopus Export 2000s. 11625.
https://stars.library.ucf.edu/scopus2000/11625