TY - GEN
T1 - L1-based model following control of an identified helicopter model in hover
AU - Picardi, Giacomo
AU - Geluardi, Stefano
AU - Olivari, Mario
AU - Pollini, Lorenzo
AU - Innocenti, Mario
AU - Bülthoff, Heinrich H.
N1 - Publisher Copyright:
© 2016 by the American Helicopter Society International, Inc. All rights reserved.
PY - 2016
Y1 - 2016
N2 - The aim of this study is to augment the uncertain dynamics of the helicopter in order to resemble the dynamics of a new kind of vehicle, the so called Personal Aerial Vehicle. To achieve this goal a two step procedure is proposed. First, the helicopter model dynamics is augmented with a PID-based dynamic controller. Such controller implements a model following on the nominal helicopter model without uncertainties. Then, an L1ad aptive controller is designed to restore the nominal responses of the augmented helicopter when variations in the identified parameters are considered. The performance of the adaptive controller is evaluated via Montecarlo simulations. The results show that the application of the adaptive controller to the augmented helicopter dynamics can significantly reduce the effects of uncertainty due to the identification of the helicopter model. For implementation reasons the adaptive controller was applied to a subset of the outputs of the system. However, the under actuation typical of helicopters makes the tracking of the nominal responses good also on the not directly adapted outputs.
AB - The aim of this study is to augment the uncertain dynamics of the helicopter in order to resemble the dynamics of a new kind of vehicle, the so called Personal Aerial Vehicle. To achieve this goal a two step procedure is proposed. First, the helicopter model dynamics is augmented with a PID-based dynamic controller. Such controller implements a model following on the nominal helicopter model without uncertainties. Then, an L1ad aptive controller is designed to restore the nominal responses of the augmented helicopter when variations in the identified parameters are considered. The performance of the adaptive controller is evaluated via Montecarlo simulations. The results show that the application of the adaptive controller to the augmented helicopter dynamics can significantly reduce the effects of uncertainty due to the identification of the helicopter model. For implementation reasons the adaptive controller was applied to a subset of the outputs of the system. However, the under actuation typical of helicopters makes the tracking of the nominal responses good also on the not directly adapted outputs.
UR - http://www.scopus.com/inward/record.url?scp=85001754609&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:85001754609
T3 - Annual Forum Proceedings - AHS International
SP - 1770
EP - 1777
BT - 72nd American Helicopter Society International Annual Forum 2016
PB - American Helicopter Society
ER -