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
  • [31] Adaptive PID Controller Using Sliding Mode Control Approaches for Quadrotor UAV Attitude and Position Stabilization
    Noordin, Aminurrashid
    Basri, Mohd Ariffanan Mohd
    Mohamed, Zaharuddin
    Lazim, Izzuddin Mat
    ARABIAN JOURNAL FOR SCIENCE AND ENGINEERING, 2021, 46 (02) : 963 - 981
  • [32] Nonlinear Disturbance Observer based Robust Attitude Tracking Controller for Quadrotor UAVs
    Lee, Kooksun
    Back, Juhoon
    Choy, Ick
    INTERNATIONAL JOURNAL OF CONTROL AUTOMATION AND SYSTEMS, 2014, 12 (06) : 1266 - 1275
  • [33] Quadrotor Tuning for Attitude Control based on Double-Loop PID Controller using Fictitious Reference Iterative Tuning (FRIT)
    Julkananusart, Arthit
    Nilkhamhang, Itthisek
    IECON 2015 - 41ST ANNUAL CONFERENCE OF THE IEEE INDUSTRIAL ELECTRONICS SOCIETY, 2015, : 4865 - 4870
  • [34] Spatial Modeling and Robust Flight Control Based on Adaptive Sliding Mode Approach for a Quadrotor MAV
    Castaneda, Herman
    Gordillo, J. L.
    JOURNAL OF INTELLIGENT & ROBOTIC SYSTEMS, 2019, 93 (1-2) : 101 - 111
  • [35] Robust Control for Attitude Tracking Problem for a Quadrotor Unmanned Aerial Vehicle
    Mokhtari, M. Rida
    Cherki, Brahim
    2013 3D INTERNATIONAL CONFERENCE ON SYSTEMS AND CONTROL (ICSC), 2013,
  • [36] Design of robust multivariable feedback control systems using pole assignment and positivity concepts
    Schmitt-Braess, G
    EUROPEAN JOURNAL OF CONTROL, 2003, 9 (04) : 384 - 391
  • [37] Robust Attitude Control based on Continuous Differentiator and Adaptive Super Twisting for 3 DOF Quadrotor
    Kahouadji, Mouad
    Braham, Amal Choukchou
    Meslouli, Ismat
    Mokhtari, M. Rida
    Cherki, Brahim
    2018 6TH INTERNATIONAL CONFERENCE ON CONTROL ENGINEERING & INFORMATION TECHNOLOGY (CEIT), 2018,
  • [38] Robust Attitude Control based on Continuous Differentiator and Adaptive Super Twisting for 3 DOF Quadrotor
    Kahouadji, Mouad
    Braham, Amal Choukchou
    Meslouli, Ismat
    Mokhtari, M. Rida
    Cherki, Brahim
    PROCEEDINGS 2018 3RD INTERNATIONAL CONFERENCE ON ELECTRICAL SCIENCES AND TECHNOLOGIES IN MAGHREB (CISTEM), 2018,
  • [39] Robust Adaptive Control based on Specified Region Pole Assignment for Flexible Hypersonic Vehicle
    Feng Zhi-gao
    MEASURING TECHNOLOGY AND MECHATRONICS AUTOMATION IV, PTS 1 AND 2, 2012, 128-129 : 270 - 275
  • [40] Quaternion-Based LQR Spacecraft Control Design Is a Robust Pole Assignment Design
    Yang, Yaguang
    JOURNAL OF AEROSPACE ENGINEERING, 2014, 27 (01) : 168 - 176