DocumentCode
622309
Title
Improving hovering performance of tethered unmanned helicopters with nonlinear control strategies
Author
Sandino, L.A. ; Bejar, M. ; Kondak, K. ; Ollero, A.
Author_Institution
GRVC, Univ. of Seville, Seville, Spain
fYear
2013
fDate
28-31 May 2013
Firstpage
443
Lastpage
452
Abstract
Hovering capabilities of unmanned helicopters can be seriously affected by wind effects. One possible solution for improving hovering performance under such circumstances is the use of a tethered setup that takes advantage of the tension exerted on the cable that links the helicopter to the ground. This paper presents a more elaborated strategy for helicopter control in this augmented setup that extends previous work on the subject by the authors. Particularly, a combination of classical PID control laws together with model inversion blocks constitutes the base of the new controller. Additionally, feed-forward action for counteracting rotational couplings is also accounted for. The resulting nonlinear control structure considers the complex and nonlinear nature of the tethered system in a better way. Several demonstrating simulations under artificially generated wind influences are presented to endorse the validity of the new proposed controller.
Keywords
aircraft control; autonomous aerial vehicles; feedforward; helicopters; three-term control; PID control law; augmented setup; cable; feed-forward action; helicopter control; hovering performance; model inversion block; nonlinear control strategy; rotational coupling; tethered setup; tethered unmanned helicopter; wind effect; Aerodynamics; Analytical models; Equations; Force; Helicopters; Mathematical model; Rotors; PID; Unmanned aerial vehicles; helicopter; model-based control; modeling; stability augmentation; tethered systems;
fLanguage
English
Publisher
ieee
Conference_Titel
Unmanned Aircraft Systems (ICUAS), 2013 International Conference on
Conference_Location
Atlanta, GA
Print_ISBN
978-1-4799-0815-8
Type
conf
DOI
10.1109/ICUAS.2013.6564719
Filename
6564719
Link To Document