A Novel Inverse Simulation Method of Helicopter Maneuvering Flight

In this article, a degeneration method of inverse simulation is proposed for a helicopter system flying pull-up and slalom maneuvers. This inverse simulation method has been successfully applied, and here, the results are compared with the flight test data and the reference data, which indicate that...

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Main Authors: Guozhi Li, Yihua Cao
Format: Article
Language:English
Published: MDPI AG 2023-06-01
Series:Applied Sciences
Subjects:
Online Access:https://www.mdpi.com/2076-3417/13/12/7214
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author Guozhi Li
Yihua Cao
author_facet Guozhi Li
Yihua Cao
author_sort Guozhi Li
collection DOAJ
description In this article, a degeneration method of inverse simulation is proposed for a helicopter system flying pull-up and slalom maneuvers. This inverse simulation method has been successfully applied, and here, the results are compared with the flight test data and the reference data, which indicate that this method has fidelity and is effective. It is different from conventional inverse simulation methods (i.e., the differentiation method and the integration method), and can improve numerical stability during inverse simulation, because the core principle is to solve the output vector in each simulation time step, by degenerating the system of first-order differential equations into nonlinear equations.
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spelling doaj.art-be289a98409c46b89e95382eadfd514a2023-11-18T09:10:42ZengMDPI AGApplied Sciences2076-34172023-06-011312721410.3390/app13127214A Novel Inverse Simulation Method of Helicopter Maneuvering FlightGuozhi Li0Yihua Cao1Chinese Aeronautical Establishment, Beijing 100029, ChinaSchool of Aeronautic Science and Engineering, Beihang University, Beijing 100191, ChinaIn this article, a degeneration method of inverse simulation is proposed for a helicopter system flying pull-up and slalom maneuvers. This inverse simulation method has been successfully applied, and here, the results are compared with the flight test data and the reference data, which indicate that this method has fidelity and is effective. It is different from conventional inverse simulation methods (i.e., the differentiation method and the integration method), and can improve numerical stability during inverse simulation, because the core principle is to solve the output vector in each simulation time step, by degenerating the system of first-order differential equations into nonlinear equations.https://www.mdpi.com/2076-3417/13/12/7214inverse simulationmaneuvering flighthelicopter
spellingShingle Guozhi Li
Yihua Cao
A Novel Inverse Simulation Method of Helicopter Maneuvering Flight
Applied Sciences
inverse simulation
maneuvering flight
helicopter
title A Novel Inverse Simulation Method of Helicopter Maneuvering Flight
title_full A Novel Inverse Simulation Method of Helicopter Maneuvering Flight
title_fullStr A Novel Inverse Simulation Method of Helicopter Maneuvering Flight
title_full_unstemmed A Novel Inverse Simulation Method of Helicopter Maneuvering Flight
title_short A Novel Inverse Simulation Method of Helicopter Maneuvering Flight
title_sort novel inverse simulation method of helicopter maneuvering flight
topic inverse simulation
maneuvering flight
helicopter
url https://www.mdpi.com/2076-3417/13/12/7214
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