Cooperative Flight Control of a Fleet of Quadrotors Using Fractional Sliding Mode With Potential Field Algorithms

被引:1
|
作者
Alabsari, Najib [1 ]
Saif, Abdul-Wahid A. [1 ,2 ,3 ]
El-Ferik, Sami [1 ,2 ]
Duffuaa, Salih [2 ,3 ]
Derbel, Nabil [4 ]
机构
[1] King Fahd Univ Petr & Minerals, Dept Control & Instrumentat Engn, Dhahran 31261, Saudi Arabia
[2] King Fahd Univ Petr & Minerals, Interdisciplinary Res Ctr Smart Mobil & Logist, Dhahran 31261, Saudi Arabia
[3] King Fahd Univ Petr & Minerals, Ind & Syst Engn Dept, Dhahran 31261, Saudi Arabia
[4] Univ Sfax, Control & Energy Management Lab CEMLab, Sfax 3038, Tunisia
关键词
Sliding mode control; fractional sliding mode control; unmanned aerial vehicle; formation control; ORDER CONTROL; TRACKING; SYSTEMS;
D O I
10.1109/ACCESS.2024.3362976
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this paper, a leader-follower-based cooperative and formation flight control is designed for a group of quadrotors using new forms of fractional sliding mode control (FSMC) strategy accompanied by the potential field algorithm. The FSMC strategy is employed as an inner controller to stabilize each individual UAV quadrotor while the potential field function is used as a formation algorithm (output controller) in order to keep a desired shape formation during the navigation of the fleet. Firstly, the stability of a single quadrotor subjected to external disturbances is addressed by designing an FSMC in addition to a classical PID controller. The FSMC is responsible for stabilizing the altitude and attitude of the vehicle while the responsibility of the PID is to control the two-dimensional (x-y) position of the UAV. Lyapunov-based sliding condition is used in the design of the fractional control strategy to guarantee system stability. The controller's parameters are tuned using the genetic algorithm (GA) to obtain better performance and more robustness against external disturbances. The potential field algorithm is used to generate the paths that are required for the fleet of vehicles to navigate while keeping a prescribed formation shape. This is done by using the attractive potential field to attract the followers toward the leader and the repulsive potential field to repulse every two neighboring followers in order to keep a required distance between them. Simulation results have proved the efficiency of the proposed control system for both the single and multi-agent cases.
引用
收藏
页码:24525 / 24543
页数:19
相关论文
共 50 条
  • [1] Cooperative Sliding Mode Control Applied To A Fleet Of DP Vessels
    Ianagui, Andre S. S.
    Tannuri, Eduardo A.
    [J]. IFAC PAPERSONLINE, 2015, 48 (16): : 299 - 304
  • [2] Multiple Quadrotors Flight Formation Control Based on Sliding Mode Control and Trajectory Tracking
    Redrovan, David Valencia
    Kim, Donghan
    [J]. 2018 INTERNATIONAL CONFERENCE ON ELECTRONICS, INFORMATION, AND COMMUNICATION (ICEIC), 2018, : 50 - 55
  • [3] Outdoor navigation using two quadrotors and adaptive sliding mode control
    Villa, Daniel K. D.
    Brandao, Alexandre S.
    Sarcinelli-Filho, Mario
    [J]. 2020 INTERNATIONAL CONFERENCE ON UNMANNED AIRCRAFT SYSTEMS (ICUAS'20), 2020, : 716 - 721
  • [4] Development of a robust attitude control for nonidentical rotor quadrotors using sliding mode control
    Promkajin, Nicom
    Parnichkun, Manukid
    [J]. INTERNATIONAL JOURNAL OF ADVANCED ROBOTIC SYSTEMS, 2018, 15 (01):
  • [5] Decentralized Cooperative Merging using Sliding Mode Control
    Rupp, Astrid
    Stolz, Michael
    Horn, Martin
    [J]. IFAC PAPERSONLINE, 2018, 51 (09): : 349 - 354
  • [6] Spacecraft swarm navigation and control using artificial potential field and sliding mode control
    Saaj, Chakravarthini M.
    Lappas, Vaios
    Gazi, Veysel
    [J]. 2006 IEEE INTERNATIONAL CONFERENCE ON INDUSTRIAL TECHNOLOGY, VOLS 1-6, 2006, : 2809 - +
  • [7] A Passive Velocity Field for Navigation of Quadrotors with Model-free Integral Sliding Mode Control
    Munoz-Vazquez, A. -J.
    Parra-Vega, V.
    Sanchez, A.
    Ramirez-Rodriguez, H.
    [J]. 2013 INTERNATIONAL CONFERENCE ON UNMANNED AIRCRAFT SYSTEMS (ICUAS), 2013, : 49 - 58
  • [8] Fractional-order integral terminal sliding-mode control for perturbed nonlinear systems with application to quadrotors
    Labbadi, Moussa
    Defoort, Michael
    Incremona, Gian Paolo
    Djemai, Mohamed
    [J]. INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL, 2023, 33 (17) : 10278 - 10303
  • [9] Attitude control of quadrotors based on fractional sliding modes: theory and experiments
    Izaguirre-Espinosa, Carlos
    Jonathan Munoz-Vazquez, Aldo
    Sanchez-Orta, Anand
    Parra-Vega, Vicente
    Castillo, Pedro
    [J]. IET CONTROL THEORY AND APPLICATIONS, 2016, 10 (07): : 825 - 832
  • [10] Optimal sliding mode flight control
    Schumacher, CJ
    Cottrill, GC
    Yeh, HH
    [J]. AIAA GUIDANCE, NAVIGATION, AND CONTROL CONFERENCE, VOLS 1-3: A COLLECTION OF TECHNICAL PAPERS, 1999, : 435 - 443