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
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;
Conference_Titel :
Unmanned Aircraft Systems (ICUAS), 2013 International Conference on
Conference_Location :
Atlanta, GA
Print_ISBN :
978-1-4799-0815-8
DOI :
10.1109/ICUAS.2013.6564719