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...
Main Authors: | , |
---|---|
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 |
_version_ | 1827738701309935616 |
---|---|
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. |
first_indexed | 2024-03-11T02:49:04Z |
format | Article |
id | doaj.art-be289a98409c46b89e95382eadfd514a |
institution | Directory Open Access Journal |
issn | 2076-3417 |
language | English |
last_indexed | 2024-03-11T02:49:04Z |
publishDate | 2023-06-01 |
publisher | MDPI AG |
record_format | Article |
series | Applied Sciences |
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 |
work_keys_str_mv | AT guozhili anovelinversesimulationmethodofhelicoptermaneuveringflight AT yihuacao anovelinversesimulationmethodofhelicoptermaneuveringflight AT guozhili novelinversesimulationmethodofhelicoptermaneuveringflight AT yihuacao novelinversesimulationmethodofhelicoptermaneuveringflight |