The paper presents the analysis on stability of digital control system for unmanned vehicle with numerical analysis. The objective of this study is mainly emphasized on the fulfillment of the advanced control techniques according to the fundamental concepts of digital control system approaches for unmanned aerial vehicle system design. The targeted unmanned aerial vehicle system was designed based on the simple construction under the idea of fixed wing flight system approaches. The stability analyses on unmanned aerial vehicle are vital role to enhance the real world applications. The background concepts on digital control system for stability analysis on dynamic control system like unmanned aerial vehicle system. The appropriate controller design for dynamic control system of unmanned aerial vehicle is vital role to analyze the accurate stability condition for reality. The implementation of numerical analysis on compensator design has been developed by using MATLAB. The physical parameters in these analyses are based on the experimental outcomes from the recent research works in dynamical system implementations. The mathematical approaches are very helpful for numerical analysis on compensator design for the unmanned aerial vehicles schemes. The simulation results confirm that the high performance stability test on unmanned aerial vehicle system has been met with the theoretical works.
| Published in | American Journal of Astronomy and Astrophysics (Volume 8, Issue 2) |
| DOI | 10.11648/j.ajaa.20200802.11 |
| Page(s) | 15-18 |
| 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), 2020. Published by Science Publishing Group |
Stability Analysis, Digital Control System, Unmanned Aerial Vehicle, Numerical Analysis, MATLAB
| [1] | Mark Edward Peterson. (2006) “The UAV and the current and future regulatory construct for integration into the national airspace system”. Journal of Air Law and Commerce, vol. 71 (5) pp. 521-612. |
| [2] | Alexander V. Koldaev. (2007) “Non-military UAV applications”. |
| [3] | T. Stastny and R. Siegwart, “Nonlinear model predictive guidance for fixed-wing uavs using identified control augmented dynamics,” in 2018 International Conference on Unmanned Aircraft Systems (ICUAS), June 2018, pp. 432–442. |
| [4] | Y. Chen, J. Liang, C. Wang, and Y. Zhang, “Combined of lyapunovstable and active disturbance rejection control for the path following of a small unmanned aerial vehicle,” International Journal of Advanced Robotic Systems, vol. 14, no. 2, 2017. |
| [5] | J. Slotine and W. Li, Applied Nonlinear Control. Prentice Hall, 1990. |
| [6] | I. Fantoni, A. Zavala, and R. Lozano, “Global stabilization of a pvtol aircraft with bounded thrust,” in Proceedings of the 41st IEEE Conference on Decision and Control, 2002., vol. 4, Dec 2002, pp. 4462–4467 vol. 4. |
| [7] | A. Flores, A. M. de Oca, and G. Flores, “A simple controller for the transition maneuver of a tail-sitter drone,” in 2018 IEEE Conference on Decision and Control (CDC), Dec 2018, pp. 4277–4281. |
| [8] | Burns, R. S. (1997) Intelligent Manufacturing, Journal of Aircraft Engineering and Aerospace Technology, MCB University Press, 69 (5), pp. 440-446. |
| [9] | Cadzow, J. A, and Martens, H. R. (1970) Discrete-Time and Computer Control Systems, Prentice-Hall, Inc., Englewood Cliffs, N. J. |
| [10] | Dorato, P. (ed) (1987) Robust Control, IEEE Press, New York. |
| [11] | Dorf, R. C. (1992) Modern Control Systems, 6th ed., Addison-Wesley, Reading, Mass. |
| [12] | Frankin, G. F., Powell, J. D. and Workman, M. L. (1990) Digital Control of Dynamic Systems, 2nd ed., Addison-Wesley, Menlow Park, CA. |
APA Style
Thanda Win, Hteik Tin Cho Nyunt, Hla Myo Tun. (2020). Stability of Digital Control System for Unmanned Aerial Vehicle with Numerical Analysis. American Journal of Astronomy and Astrophysics, 8(2), 15-18. https://doi.org/10.11648/j.ajaa.20200802.11
ACS Style
Thanda Win; Hteik Tin Cho Nyunt; Hla Myo Tun. Stability of Digital Control System for Unmanned Aerial Vehicle with Numerical Analysis. Am. J. Astron. Astrophys. 2020, 8(2), 15-18. doi: 10.11648/j.ajaa.20200802.11
AMA Style
Thanda Win, Hteik Tin Cho Nyunt, Hla Myo Tun. Stability of Digital Control System for Unmanned Aerial Vehicle with Numerical Analysis. Am J Astron Astrophys. 2020;8(2):15-18. doi: 10.11648/j.ajaa.20200802.11
Share This Article
Twitter
Linked In
Facebook
Copy
Download@article{10.11648/j.ajaa.20200802.11,
author = {Thanda Win and Hteik Tin Cho Nyunt and Hla Myo Tun},
title = {Stability of Digital Control System for Unmanned Aerial Vehicle with Numerical Analysis},
journal = {American Journal of Astronomy and Astrophysics},
volume = {8},
number = {2},
pages = {15-18},
doi = {10.11648/j.ajaa.20200802.11},
url = {https://doi.org/10.11648/j.ajaa.20200802.11},
eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.ajaa.20200802.11},
abstract = {The paper presents the analysis on stability of digital control system for unmanned vehicle with numerical analysis. The objective of this study is mainly emphasized on the fulfillment of the advanced control techniques according to the fundamental concepts of digital control system approaches for unmanned aerial vehicle system design. The targeted unmanned aerial vehicle system was designed based on the simple construction under the idea of fixed wing flight system approaches. The stability analyses on unmanned aerial vehicle are vital role to enhance the real world applications. The background concepts on digital control system for stability analysis on dynamic control system like unmanned aerial vehicle system. The appropriate controller design for dynamic control system of unmanned aerial vehicle is vital role to analyze the accurate stability condition for reality. The implementation of numerical analysis on compensator design has been developed by using MATLAB. The physical parameters in these analyses are based on the experimental outcomes from the recent research works in dynamical system implementations. The mathematical approaches are very helpful for numerical analysis on compensator design for the unmanned aerial vehicles schemes. The simulation results confirm that the high performance stability test on unmanned aerial vehicle system has been met with the theoretical works.},
year = {2020}
}
TY - JOUR T1 - Stability of Digital Control System for Unmanned Aerial Vehicle with Numerical Analysis AU - Thanda Win AU - Hteik Tin Cho Nyunt AU - Hla Myo Tun Y1 - 2020/04/17 PY - 2020 N1 - https://doi.org/10.11648/j.ajaa.20200802.11 DO - 10.11648/j.ajaa.20200802.11 T2 - American Journal of Astronomy and Astrophysics JF - American Journal of Astronomy and Astrophysics JO - American Journal of Astronomy and Astrophysics SP - 15 EP - 18 PB - Science Publishing Group SN - 2376-4686 UR - https://doi.org/10.11648/j.ajaa.20200802.11 AB - The paper presents the analysis on stability of digital control system for unmanned vehicle with numerical analysis. The objective of this study is mainly emphasized on the fulfillment of the advanced control techniques according to the fundamental concepts of digital control system approaches for unmanned aerial vehicle system design. The targeted unmanned aerial vehicle system was designed based on the simple construction under the idea of fixed wing flight system approaches. The stability analyses on unmanned aerial vehicle are vital role to enhance the real world applications. The background concepts on digital control system for stability analysis on dynamic control system like unmanned aerial vehicle system. The appropriate controller design for dynamic control system of unmanned aerial vehicle is vital role to analyze the accurate stability condition for reality. The implementation of numerical analysis on compensator design has been developed by using MATLAB. The physical parameters in these analyses are based on the experimental outcomes from the recent research works in dynamical system implementations. The mathematical approaches are very helpful for numerical analysis on compensator design for the unmanned aerial vehicles schemes. The simulation results confirm that the high performance stability test on unmanned aerial vehicle system has been met with the theoretical works. VL - 8 IS - 2 ER -
Email: