ROBUST CONTROLLER FOR SUPERSONIC UNMANNED AERIAL VEHICLE

被引:1
|
作者
Burnashev, Vitalii [1 ]
Zbrutsky, Aleksandr [1 ]
机构
[1] Natl Tech Univ Ukraine, Igor Sikorsky Kyiv Polytech Inst, Dept Aircraft Control Syst, Kiev, Ukraine
关键词
supersonic unmanned aerial vehicle; robust controller; flight trajectory; control quality; transient; controller synthesis; SYSTEM; UAV; DESIGN;
D O I
10.3846/aviation.2019.10300
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The article is devoted to the synthesis of robust controllers of supersonic unmanned aerial vehicle motion parameters. During the flight, the velocity and altitude of the aircraft varies rapidly within wide limits. Therefore, the required quality of control on each trajectory is provided by a set of dynamic controllers with constant coefficients. The article substantiates the number of such controllers, researches the range of their efficiency. The obtained restrictions on the amplitude-frequency characteristics and weight functions are given. Transients are shown.
引用
收藏
页码:31 / 35
页数:5
相关论文
共 50 条
  • [1] Robust fixed time controller with motor dynamics and composite disturbances for a quadrotor unmanned aerial vehicle
    Shang, Wei
    Hu, Shichao
    Li, Xiao
    Tu, Xikai
    INTERNATIONAL JOURNAL OF ADVANCED ROBOTIC SYSTEMS, 2020, 17 (05):
  • [2] Digital robust nonlinear controller for position and attitude stabilization of an autonomous quadrotor unmanned aerial vehicle
    Adiguzel, Fatih
    Mumcu, Tarik Veli
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2025,
  • [3] Control of a fixed wing unmanned aerial vehicle using a robust fractional order controller
    Enanwo Wondem Metekia
    Wubshet Ayalew Asfaw
    Chala Merga Abdissa
    Lebsework Negash Lemma
    Scientific Reports, 15 (1)
  • [4] Nonlinear Robust Control of a New Reconfigurable Unmanned Aerial Vehicle
    Derrouaoui, Saddam Hocine
    Bouzid, Yasser
    Guiatni, Mohamed
    ROBOTICS, 2021, 10 (02)
  • [5] Quadrotor Unmanned Aerial Vehicle Controller Design and Synthesis
    Mahfouz, M.
    Kader, Shady. A.
    2015 TENTH INTERNATIONAL CONFERENCE ON COMPUTER ENGINEERING & SYSTEMS (ICCES), 2015, : 60 - 66
  • [6] Experimental Validation of a Robust Prescribed Performance Nonlinear Controller for an Unmanned Aerial Vehicle With Unknown Mass
    Kong, Linghuan
    Reis, Joel
    He, Wei
    Silvestre, Carlos
    IEEE-ASME TRANSACTIONS ON MECHATRONICS, 2024, 29 (01) : 301 - 312
  • [7] Longitudinal Control of Small Unmanned Aerial Vehicle by PID Controller
    Pandey, Alok Kumar
    Chaudhary, Tanu
    Mishra, Shubham
    Verma, Shrestha
    INTELLIGENT COMMUNICATION, CONTROL AND DEVICES, ICICCD 2017, 2018, 624 : 923 - 931
  • [8] Altitude and attitude active disturbance rejection controller design of a quadrotor unmanned aerial vehicle
    Dou, Jingxin
    Kong, Xiangxi
    Wen, Bangchun
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2017, 231 (09) : 1732 - 1745
  • [9] A Study on Fuel Cell Electric Unmanned Aerial Vehicle
    Kaya, Kemal
    Hames, Yakup
    2019 4TH INTERNATIONAL CONFERENCE ON POWER ELECTRONICS AND THEIR APPLICATIONS (ICPEA), 2019,
  • [10] Pitch Attitude Controller Design and Simulation for a Small Unmanned Aerial Vehicle
    Huang, Chenggong
    Shao, Qiongling
    Jin, Pengfei
    Zhu, Zhen
    Zhang, Bihui
    2009 INTERNATIONAL CONFERENCE ON INTELLIGENT HUMAN-MACHINE SYSTEMS AND CYBERNETICS, VOL 2, PROCEEDINGS, 2009, : 58 - +