Theses and Dissertations

Amine Taoudi

Issuing Body

Mississippi State University

Advisor

Bhatia, Manav

Committee Member

Kim, Donghoon

Committee Member

Cheng, Yang

Date of Degree

8-10-2018

Original embargo terms

Complete embargo for 3 years

Document Type

Graduate Thesis - Open Access

Major

Aerospace Engineering

Degree Name

Master of Science

College

James Worth Bagley College of Engineering

Department

Department of Aerospace Engineering

Abstract

The vertical take-off and landing capabilities of quadrotors, and their maneuverability has contributed towards their recent popularity. They are widely used for indoors applications, where robust control strategies and automation of mission planning is necessary. In this thesis, a mathematical model for a quadrotor is derived using Newton's and Euler's laws. The model is linearized around hover and optimal control theory is used to derive a standard linear quadratic regulator controller for trajectory following. A feedorward of the tracking error is introduced to the standard LQR to improve its transient response. The performance of the proposed controller is compared with a conventional PID controller and the standard LQR controller for a variety of trajectories. The proposed controller produced a faster transient response with better disturbance rejection. A* algorithm is used to generate collisionree paths for the quadrotor where the proposed LQR is used to follow the trajectory.

URI

https://hdl.handle.net/11668/20020

Comments

LQR||A*||Path planning||PID||Quadrotor

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