Uncertainity Estimation Based Approach To Attitude Control of Fixed Wing UAV

被引：5
|
作者：
SaiCharanSagar, Andra [1 ]
Vaitheeswaran, S. M. [1 ]
Shendge, P. D. [2 ]
机构：
[1] Natl Aerosp Labs, Bangalore, Karnataka, India
[2] Coll Engn, Pune, Maharashtra, India
来源：
IFAC PAPERSONLINE | 2016年 / 49卷 / 01期
关键词：
Non linear attitude control; Backstepping(BS); Inertial delay controller(IDC); Fixed wing aircraft;
D O I：
10.1016/j.ifacol.2016.03.066
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The backstepping(BS) algorithm as a promising advanced control lacy has been combined with the inertial delay controller(DC) fat the first buns to handle time varying uncertainties and disturbances for fixed wing unmanned aerial vehicles. Other typical methods like sliding mode controller may need a relatively complex approach to handle uncertainties or under certain conditions may need a complete knowledge of the uncertainty bounds. The stability of overall system of backstepping and inertial delay controller for attitude control is proved and schemes are validated in simulations. (C) 2016, IFAC (International Federation of Automatic Control) Hosting by Elsevier Ltd. All rights reserved.
引用
收藏
页码：278 / 283
页数：6
相关论文
共 50 条
  • [1] Attitude Control of Fixed-wing UAV Based on DDQN
    Huang, Xu
    Luo, Wuyi
    Liu, Jiarun
    2019 CHINESE AUTOMATION CONGRESS (CAC2019), 2019, : 4722 - 4726
  • [2] A Complementary Filter for Attitude Estimation of a Fixed-Wing UAV
    Euston, Mark
    Coote, Paul
    Mahony, Robert
    Kim, Jonghyuk
    Hamel, Tarek
    2008 IEEE/RSJ INTERNATIONAL CONFERENCE ON ROBOTS AND INTELLIGENT SYSTEMS, VOLS 1-3, CONFERENCE PROCEEDINGS, 2008, : 340 - 345
  • [3] Attitude and altitude control for a fixed wing UAV applied to photogrammetry
    Hernandez, Jorge L.
    Gonzalez-Hernandez, Ivan
    Lozano, Rogelio
    2019 INTERNATIONAL CONFERENCE ON UNMANNED AIRCRAFT SYSTEMS (ICUAS' 19), 2019, : 498 - 502
  • [4] Modelling and Attitude Control of an Agile Fixed Wing UAV based on Nonlinear Dynamic Inversion
    Kimathi S.
    Lantos B.
    Periodica polytechnica Electrical engineering and computer science, 2022, 66 (03): : 227 - 235
  • [5] Attitude Control of Fixed Wing UAV using Multiple Sliding Surface
    Sagar, Andra Saicharan
    Shendge, P. D.
    Vaitheeswaran, S. M.
    PROCEEDINGS OF THE FIRST IEEE INTERNATIONAL CONFERENCE ON POWER ELECTRONICS, INTELLIGENT CONTROL AND ENERGY SYSTEMS (ICPEICES 2016), 2016,
  • [6] Nonlinear Extended Kalman Filter for Attitude Estimation of the Fixed-Wing UAV
    Xiaoqian, Tang
    Feicheng, Zhao
    Zhengbing, Tang
    Hongying, Wang
    International Journal of Optics, 2022, 2022
  • [7] Control of Fixed-Wing UAV Attitude and Speed based on Embedded Nonlinear Model Predictive Control
    Reinhardt, Dirk
    Johansen, Tor Arne
    IFAC PAPERSONLINE, 2021, 54 (06): : 91 - 98
  • [8] Nonlinear Extended Kalman Filter for Attitude Estimation of the Fixed-Wing UAV
    Xiaoqian, Tang
    Feicheng, Zhao
    Zhengbing, Tang
    Hongying, Wang
    INTERNATIONAL JOURNAL OF OPTICS, 2022, 2022
  • [9] Attitude control of a moving mass-actuated fixed-wing UAV based on LADRC
    Zheng, Jingzhong
    Selezneva, Maria Sergeevna
    Yi, Jianfeng
    Zhu, Liangliang
    13TH ASIA CONFERENCE ON MECHANICAL AND AEROSPACE ENGINEERING, ACMAE 2022, 2023, 2472
  • [10] Cascade PID Attitude Control Based on Adaptive Feedforward Compensation for Fixed-wing UAV
    Wang Shou-lei
    Yao Guang-le
    Chen Fang-Zheng
    PROCEEDINGS OF THE 33RD CHINESE CONTROL AND DECISION CONFERENCE (CCDC 2021), 2021, : 5006 - 5010
12345