DocumentCode
3529588
Title
Simultaneous low-order control of a nonlinear quadrotor model at four equilibria
Author
Nanjangud, Akshay
Author_Institution
Dept. of Mech. Eng., Univ. of Texas, Dallas, TX, USA
fYear
2013
fDate
10-13 Dec. 2013
Firstpage
2914
Lastpage
2919
Abstract
Four equilibria of a nonlinear quadrotor model are considered as a problem for simultaneous stabilization. Linearizations at these equilibria represent the operating modes corresponding to hover, vertical translation with any constant velocity, and horizontal translations with either any constant roll angle tilt or any constant pitch angle tilt. The linearizations at hover and vertical translation give rise to linear time-invariant systems to be stabilized. Each setting of constant roll angle or pitch angle gives rise to a different linear time-invariant system to be stabilized. Any finite number of such systems are shown be simultaneously stabilizable by simple, low-order and decentralized controllers with integral-action. Synthesis procedure for such controllers is described.
Keywords
autonomous aerial vehicles; control system synthesis; decentralised control; integral equations; linear systems; linearisation techniques; motion control; nonlinear control systems; rotors; stability; velocity control; constant pitch angle tilt; constant velocity; controller synthesis; decentralized controllers; finite number; four equilibria; horizontal translations; hover; integral-action; linear time-invariant systems; linearizations; low-order control; nonlinear quadrotor model; roll angle tilt; simultaneous stabilization; vertical translation; Aerodynamics; Aircraft; Backstepping; Force; Mathematical model; Military aircraft; Rotors;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control (CDC), 2013 IEEE 52nd Annual Conference on
Conference_Location
Firenze
ISSN
0743-1546
Print_ISBN
978-1-4673-5714-2
Type
conf
DOI
10.1109/CDC.2013.6760326
Filename
6760326
Link To Document