Predator-Prey Pigeon-Inspired Optimization for UAV ALS Longitudinal Parameters Tuning

被引:30
作者
Duan, Haibin [1 ]
Huo, Mengzhen [1 ]
Yang, Zhiyuan [1 ]
Shi, Yuhui [2 ]
Luo, Qinan [1 ]
机构
[1] Beihang Univ BUAA, Sch Automat Sci & Elect Engn, State Key Lab Virtual Real Technol Syst, Beijing 100083, Peoples R China
[2] Southern Univ Sci & Technol, Dept Comp Sci & Engn, Shenzhen Key Lab Computat Intelligence, Shenzhen 518055, Peoples R China
基金
中国国家自然科学基金;
关键词
Optimization; Aerodynamics; Unmanned aerial vehicles; Aircraft; Elevators; Heuristic algorithms; Control systems; Automatic landing; parameters tuning; predator-prey pigeon-inspired optimization (PPPIO); unmanned aerial vehicle (UAV); CONTROLLER-DESIGN; SYSTEM; GENERATION; VEHICLE;
D O I
10.1109/TAES.2018.2886612
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper presents a predator-prey pigeon-inspired optimization (PPPIO) algorithm for an automatic landing system of a fixed-wing unmanned aerial vehicle (UAV) in the longitudinal plane. Apitch command autopilot and two types of approach power compensators are presented and evaluated in automatic landing. The design of a glide slope command system and an approach power compensator are converted to a finite-dimensional optimization problem. The longitudinal flight controller parameters are optimized by the proposed PPPIO algorithm. The differences between the two proposed approach power compensators are also analyzed. The proposed optimization process can guarantee the control gains vector converge to an approximate optimal solution, and it is computationally much more efficient. Simulation results are presented to demonstrate that this approach helps solve control system optimization problems for different criteria and attains a rather accurate result. As verified by these simulation results, the proposed automatic landing system can help improve UAV's performance during the landing phase.
引用
收藏
页码:2347 / 2358
页数:12
相关论文
共 38 条
  • [1] Space-Indexed Control for Aircraft Vertical Guidance with Time Constraint
    Bouadi, Hakim
    Mora-Camino, Felix
    Choukroun, Daniel
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2014, 37 (04) : 1103 - 1113
  • [2] Robust L convex pose-graph optimisation for monocular localisation solution for unmanned aerial vehicles
    Boulekchour, Mohammed
    Aouf, Nabil
    Richardson, Mark
    [J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2015, 229 (10) : 1903 - 1918
  • [3] Campbell C. W., 1984, TRTP2313 NASA
  • [4] Trajectory Optimization of Space Maneuver Vehicle Using a Hybrid Optimal Control Solver
    Chai, Runqi
    Al Savvaris
    Tsourdos, Antonios
    Chai, Senchun
    Xia, Yuanqing
    [J]. IEEE TRANSACTIONS ON CYBERNETICS, 2019, 49 (02) : 467 - 480
  • [5] Improved Gradient-Based Algorithm for Solving Aeroassisted Vehicle Trajectory Optimization Problems
    Chai, Runqi
    Savvaris, Al
    Tsourdos, Antonios
    Chai, Senchun
    Xia, Yuanqing
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2017, 40 (08) : 2093 - 2101
  • [6] Susceptibility of F/A-18 Flight Controllers to the Falling-Leaf Mode: Linear Analysis
    Chakraborty, Abhijit
    Seiler, Peter
    Balas, Gary J.
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2011, 34 (01) : 57 - 72
  • [7] Shape optimization of airfoils in transonic flow using a multi-objective genetic algorithm
    Chen, Xiaomin
    Agarwal, Ramesh K.
    [J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2014, 228 (09) : 1654 - 1667
  • [8] Gripp JAD, 2014, INT CONF UNMAN AIRCR, P1219, DOI 10.1109/ICUAS.2014.6842378
  • [9] Control parameter design for automatic carrier landing system via pigeon-inspired optimization
    Deng, Yimin
    Duan, Haibin
    [J]. NONLINEAR DYNAMICS, 2016, 85 (01) : 97 - 106
  • [10] Ant system: Optimization by a colony of cooperating agents
    Dorigo, M
    Maniezzo, V
    Colorni, A
    [J]. IEEE TRANSACTIONS ON SYSTEMS MAN AND CYBERNETICS PART B-CYBERNETICS, 1996, 26 (01): : 29 - 41