Stability of Digital Control System for Unmanned Aerial Vehicle with Numerical Analysis

Hteik Tin Cho Nyunt,Hla Myo Tun,Thanda Win

doi:10.11648/j.ajaa.20200802.11

Hteik Tin Cho Nyunt, Hla Myo Tun + Show 1 more

Open Access

https://doi.org/10.11648/j.ajaa.20200802.11

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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.

Highlights

Unmanned aerial vehicles (UAV) are attractive progressively more prevalent as they can be used in a extensive assortment of areas
The stability test for digital control system is very important for unmanned aerial vehicle system based on numerical analysis
The dynamic control system of unmanned aerial vehicle is developed with appropriate digital controller design

Summary

Introduction

Unmanned aerial vehicles (UAV) are attractive progressively more prevalent as they can be used in a extensive assortment of areas. Multirotors are the greatest widespread, glider UAVs have supplementary benefits as their self-sufficiency is better. That is why they are applied in area for recognition or to extent additional places that multi-rotors cannot [2]. Concepts on Fixed Wing UAV and Digital Control. The Fixed-wing Unmanned Aerial Vehicles (FUAVs) have developed significant exceeding the quadrotors in remote sensing applications, fastidiousness agriculture, and reconnaissance. This is because of its aircraft survival, extensive hovering periods, extraordinary speeds and energy proficiency. Full control is well-defined as it can steady the UAV at several anticipated situation and velocity enchanting the finest angle of attack and aerodynamics [11,12]

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