DocumentCode
720463
Title
A Total Energy Control System strategy for the quadrotor helicopter
Author
Vasquez-Beltran, M.A. ; Rodriguez-Cortes, H.
Author_Institution
Centro de Investig. y de Estudios Av., Inst. Politec. Nac., Mexico City, Mexico
fYear
2015
fDate
9-12 June 2015
Firstpage
286
Lastpage
293
Abstract
This paper proposes a control strategy for the quadrotor helicopter based on the Total Energy Control System (TECS) approach. Assuming that the rotational dynamics control loop is faster than the translational dynamics control loop, a TECS based control strategy is designed for the translational dynamics. The performance of the proposed control strategy is verified experimentally.
Keywords
aircraft control; helicopters; mobile robots; power control; robot dynamics; telerobotics; quadrotor helicopter; rotational dynamics control loop; total energy control system; translational dynamics control loop; Aerodynamics; Atmospheric modeling; Helicopters; Mathematical model; Potential energy; Vehicle dynamics; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Unmanned Aircraft Systems (ICUAS), 2015 International Conference on
Conference_Location
Denver, CO
Print_ISBN
978-1-4799-6009-5
Type
conf
DOI
10.1109/ICUAS.2015.7152302
Filename
7152302
Link To Document