The Application of Rotor Control Equivalent Turbulence Input (RCETI) Models to Multi-Rotor Vehicles

This research paper investigates the applicability and scalability of the Rotor Control Equivalent Turbulence Input models for multi-rotor vehicles. Initially, a Rotor Control Equivalent Turbulence Input model is developed for an isolated rotor using rotor RPM as the input and the rotor hub-load coefficient as the output. Subsequently, the model is applied to multi-rotor vehicle example to show that the effect of turbulence on vehicle response can be replicated using the Rotor Control Equivalent Turbulence Input models. This study further incorporates rotor collective deflections, which could be used in multi-rotor vehicles, to develop a collective input model. Additionally, the effect of altering rotor parameters on the Rotor Control Equivalent Turbulence Input model is studied and presented. The results demonstrate that the Rotor Control Equivalent Turbulence Input model effectively captures the turbulence-induced behaviors in multi-rotor vehicles, offering a generalizable and scalable framework for use to replicate the effect of turbulence in multi-rotor vehicles.

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Publication Details

Journal
Aerospace
Published
2024-10-31
DOI
https://doi.org/10.3390/aerospace11110896
Primary Topic
Aerospace and Aviation Technology
Type
article
Field-Weighted Citation Impact
0.00

Funders

Controls
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article

The Application of Rotor Control Equivalent Turbulence Input (RCETI) Models to Multi-Rotor Vehicles

Mahmoud Adnan Hayajnh, J. V. R. Prasad
Aerospace
Aerospace and Aviation Technology
article

The Application of Rotor Control Equivalent Turbulence Input (RCETI) Models to Multi-Rotor Vehicles

Mahmoud Adnan Hayajnh, J. V. R. Prasad
article en

Abstract

This research paper investigates the applicability and scalability of the Rotor Control Equivalent Turbulence Input models for multi-rotor vehicles. Initially, a Rotor Control Equivalent Turbulence Input model is developed for an isolated rotor using rotor RPM as the input and the rotor hub-load coefficient as the output. Subsequently, the model is applied to multi-rotor vehicle example to show that the effect of turbulence on vehicle response can be replicated using the Rotor Control Equivalent Turbulence Input models. This study further incorporates rotor collective deflections, which could be used in multi-rotor vehicles, to develop a collective input model. Additionally, the effect of altering rotor parameters on the Rotor Control Equivalent Turbulence Input model is studied and presented. The results demonstrate that the Rotor Control Equivalent Turbulence Input model effectively captures the turbulence-induced behaviors in multi-rotor vehicles, offering a generalizable and scalable framework for use to replicate the effect of turbulence in multi-rotor vehicles.

AerospaceVol. 11(11)
Georgia Institute of Technology (US)
U.S. Army Combat Capabilities Development Command Soldier Center, U.S. Army Combat Capabilities Development Command, U.S. Army Combat Capabilities Development Command Aviation and Missile Center
Openalex Percentile: Top 70%
Aerospace and Aviation Technology
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