English

Hybrid Planning and Control for Multiple Fixed-Wing Aircraft under Input Constraints

Systems and Control 2021-06-11 v2

Abstract

This paper presents a novel hybrid control protocol for de-conflicting multiple vehicles with constraints on control inputs. We consider turning rate and linear speed constraints to represent fixed-wing or car-like vehicles. A set of state-feedback controllers along with a state-dependent switching logic are synthesized in a hybrid system to generate collision-free trajectories that converge to the desired destinations of the vehicles. The switching law is designed so that the safety can be guaranteed while no Zeno behavior can occur. A novel temporary goal assignment technique is also designed to guarantee convergence. We analyze the individual modes for safety and the closed-loop hybrid system for convergence. The theoretical developments are demonstrated via simulation results.

Keywords

Cite

@article{arxiv.1806.07328,
  title  = {Hybrid Planning and Control for Multiple Fixed-Wing Aircraft under Input Constraints},
  author = {Kunal Garg and Dimitra Panagou},
  journal= {arXiv preprint arXiv:1806.07328},
  year   = {2021}
}

Comments

Best Student Paper Finalist, AIAA-SciTech GNC Conference, 2019

R2 v1 2026-06-23T02:34:56.783Z