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Super-Twisting Sliding Mode Control with Accelerated Gradient Descent Method for Synchronous Reluctance Motor Control System Read chapter Read first chapter

2024 | OriginalPaper | Chapter

Hoist Stabilization Design Method

Authors : David Reineke, Duy (Kyle) Nguyen, Luyi Tang, M. Lanzerotti, W. Lacarbonara

Published in: Advances in Nonlinear Dynamics, Volume II

Publisher: Springer Nature Switzerland

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Abstract

Helicopter payloads for aerial evacuation (MEDEVAC) rescues are difficult to stabilize once the patient begins to swing. As a result of oscillation forces during lifting, the payload begins to swing in three dimensions under the helicopter. Swinging can pose a threat to both the crew in the helicopter and the patient attached to the cable. We first demonstrate that a payload can be stabilized in two dimensions, before exploring a three-dimensional solution. We assume that the helicopter is in a “steady hover” over the patient [1].

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Metadata
Title
Hoist Stabilization Design Method
Authors
David Reineke
Duy (Kyle) Nguyen
Luyi Tang
M. Lanzerotti
W. Lacarbonara
Copyright Year
2024
Book
Advances in Nonlinear Dynamics, Volume II

Print ISBN: 978-3-031-50638-3

Electronic ISBN: 978-3-031-50639-0

Copyright Year: 2024

DOI
https://doi.org/10.1007/978-3-031-50639-0_14

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