Motion Control analysis of a quad rotor system Part I - Experiments

被引:0
|
作者
Sidarth, S. [1 ]
Srialamelumangai, M. [1 ]
Padmapriya, R. [1 ]
Venkatesan, M. [1 ]
机构
[1] SASTRA Univ, Sch Mech Engn, Thanjavur 613401, Tamil Nadu, India
关键词
Quadcopter; stability; data acquisition; data logging; simulation;
D O I
暂无
中图分类号
TP18 [人工智能理论];
学科分类号
081104 ; 0812 ; 0835 ; 1405 ;
摘要
Quad rotors are vertical takeoff and landing systems (VTOL) which are most commonly used in surveillance, search and rescue operations, aerial photography and in automated applications. Ready to fly (RTF) quadcopter systems are now available in markets which are primarily used for various civilian applications in such a way that even a beginner without any knowledge of such systems can operate on it. The objective of the present work differs from such RTF systems. The paper focuses on assembling a quadcopter system using standard components and flying it in a stabilized manner using manual control. The stabilized flight data is acquired using a standard DAQ which is an integral part of the flying system. In part II of this work the data acquired as voltage signals which are the input to the four motors which control the flight are given as input for a mathematical model developed using MATLAB Simulink. The results of experiments carried in Part I is compared with the model developed in Part II. The logged data could be used to study the stabilization process of the flight controller which is a primary requirement for automation of the system without relying on a manual control. This will be a source for future work for complete automation of a stable flight quadcopter. The data logged during flight time is presented.
引用
收藏
页码:17 / 20
页数:4
相关论文
共 50 条
  • [41] Active model-based nonlinear system identification of quad tilt-rotor UAV with flight experiments
    Zhong Liu
    Didier Theilliol
    Yuqing He
    Feng Gu
    Liying Yang
    Jianda Han
    Science China Information Sciences, 2022, 65
  • [42] Active model-based nonlinear system identification of quad tilt-rotor UAV with flight experiments
    Zhong LIU
    Didier THEILLIOL
    Yuqing HE
    Feng GU
    Liying YANG
    Jianda HAN
    Science China(Information Sciences), 2022, (08) : 105 - 119
  • [43] Active model-based nonlinear system identification of quad tilt-rotor UAV with flight experiments
    Liu, Zhong
    Theilliol, Didier
    He, Yuqing
    Gu, Feng
    Yang, Liying
    Han, Jianda
    SCIENCE CHINA-INFORMATION SCIENCES, 2022, 65 (08)
  • [44] Dynamic analysis and vibration control of a rotor-Active magnetic bearings system with base motion
    Wu, Huachun
    Zhang, Li
    Zhou, Jian
    Hu, Yefa
    JOURNAL OF VIBRATION AND CONTROL, 2024, 30 (11-12) : 2697 - 2708
  • [45] Motion control of omnidirectional mobile manipulators (Part I) - Modeling and control
    Tan, Xiangmin
    Zhao, Dongbin
    Yi, Jianqiang
    Xu, Dong
    Jixie Gongcheng Xuebao/Journal of Mechanical Engineering, 2009, 45 (01): : 35 - 41
  • [46] Implementation of a Real-Time Attitude System for the Stabilization Control of a Quad-rotor Robot
    Barros dos Santos, Sergio Ronaldo
    Nascimento Junior, Cairo Lucio
    Givigi, Sidney N., Jr.
    Medeiros Mercante, Tiago Henrique
    Franco de Oliveira, Neusa Maria
    2013 7TH ANNUAL IEEE INTERNATIONAL SYSTEMS CONFERENCE (SYSCON 2013), 2013, : 387 - 393
  • [47] Adaptive Trajectory Tracking Control of a Quad-rotor System Based on Fuzzy Monitoring Strategy
    Song, Zhankui
    Wang, Jun
    2018 8TH INTERNATIONAL CONFERENCE ON INFORMATION SCIENCE AND TECHNOLOGY (ICIST 2018), 2018, : 415 - 421
  • [48] An adaptive control system for variable mass quad-rotor UAV involved in rescue missions
    Liang X.
    Chen G.
    Wang J.
    Bi Z.
    Sun P.
    Liang, Xiao, 1600, UK Simulation Society, Clifton Lane, Nottingham, NG11 8NS, United Kingdom (17): : 22.1 - 22.7
  • [49] Flying velocity constraint control for quad-rotor system based on finite-Time control technique
    Wei, Jiajia
    Zhou, Jun
    Du, Haibo
    Wu, Di
    PROCEEDINGS OF THE 39TH CHINESE CONTROL CONFERENCE, 2020, : 311 - 316
  • [50] Flight control system for quad-rotor aircraft based on improved integral separation PID
    Tian Hongpeng
    Li Lei
    PROCEEDINGS OF THE 2016 4TH INTERNATIONAL CONFERENCE ON MACHINERY, MATERIALS AND INFORMATION TECHNOLOGY APPLICATIONS, 2016, 71 : 582 - 586