Control augmentation strategies for helicopters used as personal aerial vehicles in low-speed regime

Carlo A. Gerboni; Joost Venrooij; Frank M. Nieuwenhuizen; Alexander Joos; Walter Fichter; Heinrich H. Bülthoff

Control augmentation strategies for helicopters used as personal aerial vehicles in low-speed regime

Carlo A. Gerboni, Joost Venrooij, Frank M. Nieuwenhuizen, Alexander Joos, Walter Fichter, Heinrich H. Bülthoff

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Abstract

In this paper an augmentation strategy is implemented with the goal of making the behavior of an actual helicopter similar to that of a new class of aerial systems called Personal Aerial Vehicles (PAVs). PAVs are meant to be own by flight-naïve pilots, i.e., pilots with minimal flight experience. One feature required for achieving this goal, is to have a Translation Rate Command (TRC) response type in the hover and low-speed regime. In this paper, a TRC response type is obtained for a UH-60 helicopter simulation model in hover and low-speed regime through the implementation of nonlinear back stepping control. The responses of the rotorcraft with TRC response type are evaluated with the metrics defined in the Aeronautical Design Standard ADS-33. E-PRF. Simulations show the efficiency of the control scheme in tracking the reference velocities and the achievement of the requirements to have level 1 Handling Qualities (HQ) for the TRC response type.

Original language	English
Title of host publication	AIAA Modeling and Simulation Technologies Conference
Publisher	American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)	9781624103872
Publication status	Published - 2016
Event	AIAA Modeling and Simulation Technologies Conference, 2016 - San Diego, United States Duration: 2016 Jan 4 → 2016 Jan 8

Publication series

Name	AIAA Modeling and Simulation Technologies Conference

Other

Other	AIAA Modeling and Simulation Technologies Conference, 2016
Country/Territory	United States
City	San Diego
Period	16/1/4 → 16/1/8

Bibliographical note

Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc. All rights reserved.

Copyright:
Copyright 2016 Elsevier B.V., All rights reserved.

ASJC Scopus subject areas

Aerospace Engineering
Modelling and Simulation

Cite this

Gerboni, C. A., Venrooij, J., Nieuwenhuizen, F. M., Joos, A., Fichter, W., & Bülthoff, H. H. (2016). Control augmentation strategies for helicopters used as personal aerial vehicles in low-speed regime. In AIAA Modeling and Simulation Technologies Conference (AIAA Modeling and Simulation Technologies Conference). American Institute of Aeronautics and Astronautics Inc, AIAA.

Control augmentation strategies for helicopters used as personal aerial vehicles in low-speed regime. / Gerboni, Carlo A.; Venrooij, Joost; Nieuwenhuizen, Frank M. et al.
AIAA Modeling and Simulation Technologies Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, 2016. (AIAA Modeling and Simulation Technologies Conference).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Gerboni, CA, Venrooij, J, Nieuwenhuizen, FM, Joos, A, Fichter, W & Bülthoff, HH 2016, Control augmentation strategies for helicopters used as personal aerial vehicles in low-speed regime. in AIAA Modeling and Simulation Technologies Conference. AIAA Modeling and Simulation Technologies Conference, American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA Modeling and Simulation Technologies Conference, 2016, San Diego, United States, 16/1/4.

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abstract = "In this paper an augmentation strategy is implemented with the goal of making the behavior of an actual helicopter similar to that of a new class of aerial systems called Personal Aerial Vehicles (PAVs). PAVs are meant to be own by flight-na{\"i}ve pilots, i.e., pilots with minimal flight experience. One feature required for achieving this goal, is to have a Translation Rate Command (TRC) response type in the hover and low-speed regime. In this paper, a TRC response type is obtained for a UH-60 helicopter simulation model in hover and low-speed regime through the implementation of nonlinear back stepping control. The responses of the rotorcraft with TRC response type are evaluated with the metrics defined in the Aeronautical Design Standard ADS-33. E-PRF. Simulations show the efficiency of the control scheme in tracking the reference velocities and the achievement of the requirements to have level 1 Handling Qualities (HQ) for the TRC response type.",

author = "Gerboni, {Carlo A.} and Joost Venrooij and Nieuwenhuizen, {Frank M.} and Alexander Joos and Walter Fichter and B{\"u}lthoff, {Heinrich H.}",

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AU - Gerboni, Carlo A.

AU - Venrooij, Joost

AU - Nieuwenhuizen, Frank M.

AU - Joos, Alexander

AU - Fichter, Walter

AU - Bülthoff, Heinrich H.

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AB - In this paper an augmentation strategy is implemented with the goal of making the behavior of an actual helicopter similar to that of a new class of aerial systems called Personal Aerial Vehicles (PAVs). PAVs are meant to be own by flight-naïve pilots, i.e., pilots with minimal flight experience. One feature required for achieving this goal, is to have a Translation Rate Command (TRC) response type in the hover and low-speed regime. In this paper, a TRC response type is obtained for a UH-60 helicopter simulation model in hover and low-speed regime through the implementation of nonlinear back stepping control. The responses of the rotorcraft with TRC response type are evaluated with the metrics defined in the Aeronautical Design Standard ADS-33. E-PRF. Simulations show the efficiency of the control scheme in tracking the reference velocities and the achievement of the requirements to have level 1 Handling Qualities (HQ) for the TRC response type.

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T2 - AIAA Modeling and Simulation Technologies Conference, 2016

Y2 - 4 January 2016 through 8 January 2016

ER -

Control augmentation strategies for helicopters used as personal aerial vehicles in low-speed regime

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ASJC Scopus subject areas

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