Version 1
: Received: 19 July 2023 / Approved: 19 July 2023 / Online: 20 July 2023 (07:50:16 CEST)
How to cite:
Liu, Z.; Xiang, L.; Zhu, Z. Cooperative Standoff Target Tracking using Multiple Fixed-wing UAVs with Input Constraints in Unknown Wind. Preprints2023, 2023071347. https://doi.org/10.20944/preprints202307.1347.v1
Liu, Z.; Xiang, L.; Zhu, Z. Cooperative Standoff Target Tracking using Multiple Fixed-wing UAVs with Input Constraints in Unknown Wind. Preprints 2023, 2023071347. https://doi.org/10.20944/preprints202307.1347.v1
Liu, Z.; Xiang, L.; Zhu, Z. Cooperative Standoff Target Tracking using Multiple Fixed-wing UAVs with Input Constraints in Unknown Wind. Preprints2023, 2023071347. https://doi.org/10.20944/preprints202307.1347.v1
APA Style
Liu, Z., Xiang, L., & Zhu, Z. (2023). Cooperative Standoff Target Tracking using Multiple Fixed-wing UAVs with Input Constraints in Unknown Wind. Preprints. https://doi.org/10.20944/preprints202307.1347.v1
Chicago/Turabian Style
Liu, Z., Lingshuang Xiang and Zemin Zhu. 2023 "Cooperative Standoff Target Tracking using Multiple Fixed-wing UAVs with Input Constraints in Unknown Wind" Preprints. https://doi.org/10.20944/preprints202307.1347.v1
Abstract
This paper investigates the problem of cooperative standoff tracking using multiple fixed-wing unmanned aerial vehicles (UAVs) with control input constraints. In order to achieve accurate target tracking in the presence of unknown background wind and target motion, a coordinated standoff target tracking algorithm is proposed. The objective of the research is to steer multiple UAVs to fly a circular orbit around a moving target with prescribed intervehicle angular spacing. To achieve this goal, two control laws are proposed, including relative range regulation and space phase separation. On one hand, a heading rate control law based on Lyapunov guidance vector field is proposed. The convergence analysis show that the UAVs can asymptotically converge to a desired circular orbit around the target, regardless of their initial position and heading. Through rigorous theoretical proof, it is concluded that the command signal of the proposed heading rate controller will not violate the boundary constraint on heading rate. On the other hand, a temporal phase is introduced to represent the phase separation and avoid discontinuity of the wrapped space phase angle. On this basis, a speed controller is developed to achieve equal phase separation. The proposed airspeed controller met the requirement of airspeed constraint. In addition, to improve the robustness of the aircraft during target tracking, an estimator is developed to estimate the composition velocity of the unknown wind and target motion. The proposed estimator uses the offset vector between the UAV’s actual flight path and the desired orbit which is defined by Lyapunov guidance vector field to estimate the composition velocity. The stability of the estimator is proved. Simulations are conducted under different scenarios to demonstrate the effectiveness of the proposed cooperative standoff target tracking algorithm. The simulation results of indicate that, the temporal-phase-based speed controller can achieve fast convergence speed and small phase separation error. Additionally, the composition velocity estimator exhibits fast response speed and high estimation accuracy.
Copyright:
This is an open access article distributed under the Creative Commons Attribution License which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
