Design and simulation of stabilized flight controller for UAVs

Ismat Hira; Intesar Ahmed; Hira Akash; Amna Naqvi; Iqra Manzoor; Mehak Jahangir

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Design and simulation of stabilized flight controller for UAVs

Author(s)

Ismat Hira Department of Electrical Engineering, Lahore College for Women University, Lahore, Pakistan

Intesar Ahmed Department of Electrical Engineering, Lahore College for Women University, Lahore, Pakistan

Hira Akash Department of Electrical Engineering, Lahore College for Women University, Lahore, Pakistan

Amna Naqvi Department of Electrical Engineering, Lahore College for Women University, Lahore, Pakistan

Iqra Manzoor Department of Electrical Engineering, Lahore College for Women University, Lahore, Pakistan

Mehak Jahangir Department of Electrical Engineering, Lahore College for Women University, Lahore, Pakistan

Abstract

This research paper is based on modeling and simulation of Unmanned Aerial Vehicles (UAVs) system using the equation of motion for stability and signal regulation. Two controllers have been used in sequence, Linear Quadratic Controller (LQR) and Proportional, Integral, Derivative (PID) for stability and signal regulation respectively. With the use of LQR, the system becomes more stable and less sensitive. This research work is divided into four parts i.e. mathematical modeling, design procedure of LQR and PID controllers, simulation and results. DATCOM files are imported by using datcom function. The results obtained from these simulations based on stability and signal regulation of UAVsystem.

Publication Details

Page(s) 17-22

DOI DOI not available

Published Journal: New Horizons: Journal of the Institution of Electrical & Electronics Engineers Pakistan, Volume: 88, Issue: 0, Year: 2015

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