American Journal of Astronomy and Astrophysics

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Robust Performance Analysis on Dynamic Control of Unmanned Aerial Vehicle System Using Bode Plot

Received: Oct. 19, 2019    Accepted: Nov. 14, 2019    Published: Nov. 25, 2019
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Abstract

The paper focuses on the robust performance analysis on dynamic control of unmanned aerial vehicle system with numerical computation. The objectives of this work are to find the appropriate solution for robust stability problems for dynamic control of unmanned aerial vehicle (UAV) system which is critical challenge in the space technology. The background of the theoretical work on digital control system is very important to study the problem of dynamic control system at present. The idea behind the control system stability analysis on digital technology is very important candidate in space technology. The specific purpose on analyzing the performance of dynamic of digital control system for space technology is solved in this paper. The mathematical model of target system is mentioned and analyzed based on the classical control method with digital technology. The related work for modeling of the control system is mentioned and expressed the detailed background for the analysis. The simulation results confirm that the proposed system met the robust performance for digital control of UAV system for reality. The analysis has been carried out based on feedback control system stability for dynamic system as well. The simulation results for stability analysis have been carried out by using MATLAB programming languages.

DOI 10.11648/j.ajaa.20190704.11
Published in American Journal of Astronomy and Astrophysics ( Volume 7, Issue 4, December 2019 )
Page(s) 48-53
Creative Commons

This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited.

Copyright

Copyright © The Author(s), 2024. Published by Science Publishing Group

Keywords

Robust Performance, Dynamic Control, Unmanned Aerial Vehicle, Numerical Analysis, MATLAB

References
[1] Burns, R. S. (1997) Intelligent Manufacturing, Journal of Aircraft Engineering and Aerospace Technology, MCB University Press, 69 (5), pp. 440-446.
[2] Cadzow, J. A, and Martens, H. R. (1970) Discrete-Time and Computer Control Systems, Prentice-Hall, Inc., Englewood Cliffs, N. J.
[3] Dorato, P. (ed) (1987) Robust Control, IEEE Press, New York.
[4] Dorf, R. C. (1992) Modern Control Systems, 6th ed., Addison-Wesley, Reading, Mass.
[5] Frankin, G. F., Powell, J. D. and Workman, M.L. (1990) Digital Control of Dynamic Systems, 2nd ed., Addison-Wesley, Menlow Park, CA.
[6] B. Yang; Y. X. Xu ; Q. F. Hu ; B. Yang; C. Y. Xing; X. Rui, Reserch on digital closed-loop control for silicon resonant accelerometer, 2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) , St. Petersburg, Russia.
[7] Mingming Yin; Serhiy Bozhko; Taike Yao; Chengxin You, Control System Design and the Power Management of MEFADEC Assembled on More-Electric Aircraft, 2018 IEEE International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles & International Transportation Electrification Conference (ESARS-ITEC), Nottingham, UK.
[8] Nitesh Agrawal; Susovon Samanta, Development of System-On-Chip Based Digital Control for Power Converter Application, 2018 IEEE International Conference on Power Electronics, Drives and Energy Systems (PEDES), Chennai, India, India.
[9] Maogui Niu; Yong Zhou; Long Chen; Yanting Han; Yanzhao Mi; Chao Zhang, Research on Servo Control System of Electromechanical Actuators with Compound Control and Three Closed-Loop, 2018 International Conference on Sensing, Diagnostics, Prognostics, and Control (SDPC), Xi'an, China, China.
[10] Jijun Xue; Miao Yu; Xiumei Du; Xiaoying Xu; Jie Fu; Zhiwei Xing, Design and implementation of the control system for magnetorheological suspension of all-terrain vehicle, 2018 Chinese Control And Decision Conference (CCDC), Shenyang, China.
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  • APA Style

    Hteik Tin Cho Nyunt, Thanda Win, Hla Myo Tun. (2019). Robust Performance Analysis on Dynamic Control of Unmanned Aerial Vehicle System Using Bode Plot. American Journal of Astronomy and Astrophysics, 7(4), 48-53. https://doi.org/10.11648/j.ajaa.20190704.11

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    ACS Style

    Hteik Tin Cho Nyunt; Thanda Win; Hla Myo Tun. Robust Performance Analysis on Dynamic Control of Unmanned Aerial Vehicle System Using Bode Plot. Am. J. Astron. Astrophys. 2019, 7(4), 48-53. doi: 10.11648/j.ajaa.20190704.11

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    AMA Style

    Hteik Tin Cho Nyunt, Thanda Win, Hla Myo Tun. Robust Performance Analysis on Dynamic Control of Unmanned Aerial Vehicle System Using Bode Plot. Am J Astron Astrophys. 2019;7(4):48-53. doi: 10.11648/j.ajaa.20190704.11

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  • @article{10.11648/j.ajaa.20190704.11,
      author = {Hteik Tin Cho Nyunt and Thanda Win and Hla Myo Tun},
      title = {Robust Performance Analysis on Dynamic Control of Unmanned Aerial Vehicle System Using Bode Plot},
      journal = {American Journal of Astronomy and Astrophysics},
      volume = {7},
      number = {4},
      pages = {48-53},
      doi = {10.11648/j.ajaa.20190704.11},
      url = {https://doi.org/10.11648/j.ajaa.20190704.11},
      eprint = {https://download.sciencepg.com/pdf/10.11648.j.ajaa.20190704.11},
      abstract = {The paper focuses on the robust performance analysis on dynamic control of unmanned aerial vehicle system with numerical computation. The objectives of this work are to find the appropriate solution for robust stability problems for dynamic control of unmanned aerial vehicle (UAV) system which is critical challenge in the space technology. The background of the theoretical work on digital control system is very important to study the problem of dynamic control system at present. The idea behind the control system stability analysis on digital technology is very important candidate in space technology. The specific purpose on analyzing the performance of dynamic of digital control system for space technology is solved in this paper. The mathematical model of target system is mentioned and analyzed based on the classical control method with digital technology. The related work for modeling of the control system is mentioned and expressed the detailed background for the analysis. The simulation results confirm that the proposed system met the robust performance for digital control of UAV system for reality. The analysis has been carried out based on feedback control system stability for dynamic system as well. The simulation results for stability analysis have been carried out by using MATLAB programming languages.},
     year = {2019}
    }
    

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    AU  - Hteik Tin Cho Nyunt
    AU  - Thanda Win
    AU  - Hla Myo Tun
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    DO  - 10.11648/j.ajaa.20190704.11
    T2  - American Journal of Astronomy and Astrophysics
    JF  - American Journal of Astronomy and Astrophysics
    JO  - American Journal of Astronomy and Astrophysics
    SP  - 48
    EP  - 53
    PB  - Science Publishing Group
    SN  - 2376-4686
    UR  - https://doi.org/10.11648/j.ajaa.20190704.11
    AB  - The paper focuses on the robust performance analysis on dynamic control of unmanned aerial vehicle system with numerical computation. The objectives of this work are to find the appropriate solution for robust stability problems for dynamic control of unmanned aerial vehicle (UAV) system which is critical challenge in the space technology. The background of the theoretical work on digital control system is very important to study the problem of dynamic control system at present. The idea behind the control system stability analysis on digital technology is very important candidate in space technology. The specific purpose on analyzing the performance of dynamic of digital control system for space technology is solved in this paper. The mathematical model of target system is mentioned and analyzed based on the classical control method with digital technology. The related work for modeling of the control system is mentioned and expressed the detailed background for the analysis. The simulation results confirm that the proposed system met the robust performance for digital control of UAV system for reality. The analysis has been carried out based on feedback control system stability for dynamic system as well. The simulation results for stability analysis have been carried out by using MATLAB programming languages.
    VL  - 7
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Author Information
  • Department of Electronic Engineering, Government Technical High School (Shwe Pyi Thar), Yangon Region, Republic of the Union of Myanmar

  • Department of Electronic Engineering, West Yangon Technological University, Yangon Region, Republic of the Union of Myanmar

  • Department of Electronic Engineering, Yangon Technological University, Yangon Region, Republic of the Union of Myanmar

  • Section