Longitudinal parameter identification of a small unmanned aerial vehicle based on modified particle swarm optimization

被引:27
作者
Jiang Tieying [1 ]
Li Jie [1 ]
Huang Kewei [1 ]
机构
[1] Beijing Inst Technol, Coll Mech & Elect Engn, Beijing 100081, Peoples R China
关键词
Aerodynamic parameters; Local optimization; Parameter identification; Particle swarm optimization (PSO); Small unmanned aerial vehicle; SYSTEM-IDENTIFICATION; ALGORITHM;
D O I
10.1016/j.cja.2015.04.005
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper describes a longitudinal parameter identification procedure for a small unmanned aerial vehicle (UAV) through modified particle swam optimization (PSO). The procedure is demonstrated using a small UAV equipped with only an micro-electro-mechanical systems (MEMS) inertial measuring element and a global positioning system (GPS) receiver to provide test information. A small UAV longitudinal parameter mathematical model is derived and the modified method is proposed based on PSO with selective particle regeneration (SRPSO). Once modified PSO is applied to the mathematical model, the simulation results show that the mathematical model is correct, and aerodynamic parameters and coefficients of the propeller can be identified accurately. Results are compared with those of PSO and SRPSO and the comparison shows that the proposed method is more robust and faster than the other methods for the longitudinal parameter identification of the small UAV. Some parameter identification results are affected slightly by noise, but the identification results are very good overall. Eventually, experimental validation is employed to test the proposed method, which demonstrates the usefulness of this method. (C) 2015 The Authors. Production and hosting by Elsevier Ltd. on behalf of CSAA & BUAA. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).
引用
收藏
页码:865 / 873
页数:9
相关论文
共 27 条
  • [1] Expert algorithm based on adaptive particle swarm optimization for power flow analysis
    Acharjee, P.
    Goswami, S. K.
    [J]. EXPERT SYSTEMS WITH APPLICATIONS, 2009, 36 (03) : 5151 - 5156
  • [2] Aerodynamic parameter identification for symmetric projectiles: An improved gradient based method
    Burchett, Bradley T.
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 30 (01) : 119 - 127
  • [3] CAI JF, 1995, ADV TXB TRADITIONAL, P10
  • [4] Chi-Yang Tsai, 2009, WSEAS Transactions on Information Science and Applications, V6, P242
  • [5] System Identification for Small, Low-Cost, Fixed-Wing Unmanned Aircraft
    Dorobantu, Andrei
    Murch, Austin
    Mettler, Berenice
    Balas, Gary
    [J]. JOURNAL OF AIRCRAFT, 2013, 50 (04): : 1117 - 1130
  • [6] Ducard GJJ, 2009, ADV IND CONTROL, P1
  • [7] Hall J, 2006, AIAA20066689
  • [8] Hatamleh KS, 2010, THESIS NEW MEXICO ST
  • [9] A hybridized approach to data clustering
    Kao, Yi-Tung
    Zahara, Erwie
    Kao, I-Wei
    [J]. EXPERT SYSTEMS WITH APPLICATIONS, 2008, 34 (03) : 1754 - 1762
  • [10] Kennedy J, 1995, 1995 IEEE INTERNATIONAL CONFERENCE ON NEURAL NETWORKS PROCEEDINGS, VOLS 1-6, P1942, DOI 10.1109/icnn.1995.488968