PID-based attitude control of quadrotor using robust pole assignment and LPV modeling

被引:3
|
作者
Kazemi, Mohammad Hossein [1 ]
Tarighi, Reza [2 ]
机构
[1] Shahed Univ, Dept Elect Engn, Persian Gulf Hwy, Tehran 3319118651, Iran
[2] Islamic Azad Univ, Dept Control Engn, Fac Elect Engn, Tehran, Iran
关键词
LMI; Polytopic LPV modeling; Quadrotor dynamics; Robust control; ALGORITHMS; TRACKING; POSITION; DESIGN; UAV;
D O I
10.1007/s40435-023-01372-6
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
A novel control strategy is addressed in this paper for tracking control of a Quadrotor attitude based on PID structure. The nonlinear model of quadrotor including gyroscopic effects is considered for a Polytopic Linear Parameter Varying (LPV) modeling. Specifically, the control scheme adopted combines three techniques. On the one hand, the convex LPV controller using the nonlinearity approach has the advantage of precisely describing the system's nonlinear behavior by interpolating local linear models, and one can extrapolate linear controller designs to the nonlinear case considering a more realistic scenario. The principle component analysis (PCA)-based parameter set mapping is used for creating a low dimensional Polytopic LPV model. Augmenting the proposed PID-based control action states to the plant states results in an overall plant in the form of standard robust state feedback control problem where a robust pole assignment controller is designed. An H infinity attenuation level for the tracking error under external disturbances such as wind effects is guaranteed by solving the introduced linear matrix inequalities (LMIs) to compute the control gains. Simulating the planned controller to a proposed quadrotor shows the effectiveness of the proposed strategy in attitude control problem against the external disturbances.
引用
收藏
页码:2385 / 2397
页数:13
相关论文
共 50 条
  • [1] Research on Attitude Control Algorithm of PID Quadrotor based on LPV Method
    Hu, Chenyu
    Yang, Hui
    PROCEEDINGS OF THE 2ND INTERNATIONAL CONFERENCE ON MECHATRONICS ENGINEERING AND INFORMATION TECHNOLOGY (ICMEIT 2017), 2017, 70 : 569 - 576
  • [2] Modeling and Robust Attitude Control of a Quadrotor System
    Torres Gaitan, Angelica
    Bolea, Yolanda
    2013 10TH INTERNATIONAL CONFERENCE ON ELECTRICAL ENGINEERING, COMPUTING SCIENCE AND AUTOMATIC CONTROL (CCE), 2013, : 7 - 12
  • [3] Quadrotor helicopter Attitude Control using cascade PID
    Bo, Gaopeng
    Xin, Liuyong
    Hui, Zhang
    Ling, Wanglin
    PROCEEDINGS OF THE 28TH CHINESE CONTROL AND DECISION CONFERENCE (2016 CCDC), 2016, : 5158 - 5163
  • [4] Attitude control of a quadrotor using PID controller based on differential evolution algorithm
    Gun, Ayhan
    EXPERT SYSTEMS WITH APPLICATIONS, 2023, 229
  • [5] Attitude Control of Quadrotor in Consideration of the Effects of a Pole Based on Limited Pole Placement
    Sugawara, Yasunori
    Shimada, Akira
    ELECTRICAL ENGINEERING IN JAPAN, 2017, 198 (01) : 34 - 44
  • [6] Robust stability check for fractional PID-based control systems
    Moornani, Kamran Akbari
    Haeri, Mohammad
    TRANSACTIONS OF THE INSTITUTE OF MEASUREMENT AND CONTROL, 2013, 35 (02) : 236 - 246
  • [7] EKF-AF PID-Based Attitude Control Algorithm for UAVs
    Song, He
    Hu, Shaolin
    Jiang, Wenqiang
    Guo, Qiliang
    MOBILE INFORMATION SYSTEMS, 2022, 2022
  • [8] Robust Cascade PID Attitude Control of Quadrotor Helicopters Subject to Wind Disturbance
    Zhou, Jie
    Deng, Ruiliang
    Shi, Zongying
    Zhong, Yisheng
    PROCEEDINGS OF THE 36TH CHINESE CONTROL CONFERENCE (CCC 2017), 2017, : 6558 - 6563
  • [9] Robust Attitude Control of Quadrotor using Sliding Mode
    Dey, Parthibi
    Kurode, Shailaja R.
    Ramachandran, Raghu
    2016 INTERNATIONAL CONFERENCE ON AUTOMATIC CONTROL AND DYNAMIC OPTIMIZATION TECHNIQUES (ICACDOT), 2016, : 268 - 272
  • [10] Smith predictor PID-based robust adaptive gain-scheduled control for a class of fractional order LPV systems with time delays
    Kissoum, Safia
    Ladaci, Samir
    Charef, Abdelfatah
    INTERNATIONAL JOURNAL OF DYNAMICS AND CONTROL, 2023, 11 (6) : 3096 - 3108