Attitude Control of Fixed Wing UAV using Multiple Sliding Surface

被引：0
|
作者：
Sagar, Andra Saicharan [1 ]
Shendge, P. D. [2 ]
Vaitheeswaran, S. M. [3 ]
机构：
[1] Coll Engn, Nat Aerosp Labs, Pune, Maharashtra, India
[2] Coll Engn, Dept Instrumentat & Control, Pune, Maharashtra, India
[3] CSIR, Natl Aerosp Labs, Aerosp Elect & Syst Div, Bangalore, Karnataka, India
来源：
PROCEEDINGS OF THE FIRST IEEE INTERNATIONAL CONFERENCE ON POWER ELECTRONICS, INTELLIGENT CONTROL AND ENERGY SYSTEMS (ICPEICES 2016) | 2016年
关键词：
Fixed Wing Unmanned Aircraft; Sliding Mode Controller (SMC); Multiple Sliding Surface Controller (MSSC); Inertial Delay Controller (IDC); FLIGHT CONTROL; SYSTEMS;
D O I：
暂无
中图分类号：
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号：
0807 ; 0820 ;
摘要：
A design method for controlling the attitude of a fixed wing aircraft in the presence of uncertainties is proposed in the Multiple Sliding Surface framework. Inertial Delay Controller is integrated with Multiple Sliding surface Controller to increase the performance of system by estimating the uncertainties that are present in the system.
引用
收藏
页数：6
相关论文
共 50 条
  • [31] Backstepping - Sliding Mode Controllers Applied to a Fixed-Wing UAV
    T. Espinoza
    A. E. Dzul
    R. Lozano
    P. Parada
    Journal of Intelligent & Robotic Systems, 2014, 73 : 67 - 79
  • [32] Backstepping - Sliding Mode Controllers Applied to a Fixed-Wing UAV
    Espinoza, T.
    Dzul, A. E.
    Lozano, R.
    Parada, P.
    JOURNAL OF INTELLIGENT & ROBOTIC SYSTEMS, 2014, 73 (1-4) : 67 - 79
  • [33] Backstepping - sliding mode controllers applied to a fixed-wing UAV
    Espinoza, T.
    Dzul, A.
    Lozano, R.
    Parada, P.
    2013 INTERNATIONAL CONFERENCE ON UNMANNED AIRCRAFT SYSTEMS (ICUAS), 2013, : 95 - 104
  • [34] Attitude Control of a Class of Fixed-Wing UAV with Wiener Noises Based on Barrier Lyapunov Function
    Sun, Gonghao
    Guo, Yunhe
    Xu, Shengli
    Zhang, Di
    Bai, Yu
    PROCEEDINGS OF 2022 INTERNATIONAL CONFERENCE ON AUTONOMOUS UNMANNED SYSTEMS, ICAUS 2022, 2023, 1010 : 1515 - 1524
  • [35] Design of a Fixed-Wing UAV Controller Combined Fuzzy Adaptive Method and Sliding Mode Control
    Guo, Yufei
    Luo, Leru
    Bao, Changchun
    MATHEMATICAL PROBLEMS IN ENGINEERING, 2022, 2022
  • [36] Design of a Fixed-Wing UAV Controller Based on Adaptive Backstepping Sliding Mode Control Method
    Bao, Changchun
    Guo, Yufei
    Luo, Leru
    Su, Guanqun
    IEEE ACCESS, 2021, 9 (09): : 157825 - 157841
  • [37] Position and Attitude control of a Quadrotor UAV using Super Twisting Sliding Mode
    Jayakrishnan, H. J.
    IFAC PAPERSONLINE, 2016, 49 (01): : 284 - 289
  • [38] Stability Control of Small Fixed-Wing UAV
    Cheng, Yuan
    Xu, Shouzhi
    Huang, Zhiyong
    Xiong, Biao
    Wang, Chao
    2014 11TH WORLD CONGRESS ON INTELLIGENT CONTROL AND AUTOMATION (WCICA), 2014, : 1056 - 1060
  • [39] Guidance, Navigation, and Control for Fixed-Wing UAV
    Israr, Amber
    Alkhammash, Eman H.
    Hadjouni, Myriam
    MATHEMATICAL PROBLEMS IN ENGINEERING, 2021, 2021
  • [40] Dynamic modeling and control of tilting fixed wing UAV
    Zhang Y.
    Deng Y.
    Liu Y.
    Huazhong Keji Daxue Xuebao (Ziran Kexue Ban)/Journal of Huazhong University of Science and Technology (Natural Science Edition), 2019, 47 (08): : 98 - 102
12345