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 :
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