Keen Investigation of the Electromagnetic Scattering Characteristics of Tiltrotor Aircraft Based on Dynamic Calculation Method

To study the radar characteristics of the tiltrotor aircraft when considering rotor rotation and tilting actions, a dynamic calculation method (DCM) based on physical optics and physical theory of diffraction is presented. The results show that the radar cross section of a single rotor is dynamic an...

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Main Authors: Zeyang Zhou, Jun Huang, Chen Chen, Jiaren Zhang
Format: Article
Language:English
Published: MDPI AG 2021-05-01
Series:Photonics
Subjects:
Online Access:https://www.mdpi.com/2304-6732/8/6/175
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spelling doaj-ff4c97810b134a468aca386df5cb16c32021-06-01T00:46:37ZengMDPI AGPhotonics2304-67322021-05-01817517510.3390/photonics8060175Keen Investigation of the Electromagnetic Scattering Characteristics of Tiltrotor Aircraft Based on Dynamic Calculation MethodZeyang Zhou0Jun Huang1Chen Chen2Jiaren Zhang3School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, ChinaSchool of Aeronautic Science and Engineering, Beihang University, Beijing 100191, ChinaHIWING Aviation General Equipment Corporation Limited, Beijing 100074, ChinaAVIC SAC Commercial Aircraft Company Limited, Shenyang 110179, ChinaTo study the radar characteristics of the tiltrotor aircraft when considering rotor rotation and tilting actions, a dynamic calculation method (DCM) based on physical optics and physical theory of diffraction is presented. The results show that the radar cross section of a single rotor is dynamic and periodic when it rotates, while increasing the rotation speed can shorten this period. At a fixed tilt angle, the overall radar cross section of the cabin plus rotor still exhibits various dynamic characteristics at different azimuths when considering the rotation of the rotor. Increasing the tilt angle can better improve the electromagnetic scattering level of the rotor, but this easily makes the cabin and the outer end of the wing become a new source of strong scattering. In the heading direction, the dynamic radar cross section of the aircraft under a larger azimuth angle is lower when the cabin tilts from horizontal to vertical position. The presented DCM is feasible and effective to obtain the electromagnetic scattering characteristics of tiltrotor aircraft.https://www.mdpi.com/2304-6732/8/6/175tiltrotor aircraftradar stealthdynamic electromagnetic scatteringradar cross-section
collection DOAJ
language English
format Article
sources DOAJ
author Zeyang Zhou
Jun Huang
Chen Chen
Jiaren Zhang
spellingShingle Zeyang Zhou
Jun Huang
Chen Chen
Jiaren Zhang
Keen Investigation of the Electromagnetic Scattering Characteristics of Tiltrotor Aircraft Based on Dynamic Calculation Method
Photonics
tiltrotor aircraft
radar stealth
dynamic electromagnetic scattering
radar cross-section
author_facet Zeyang Zhou
Jun Huang
Chen Chen
Jiaren Zhang
author_sort Zeyang Zhou
title Keen Investigation of the Electromagnetic Scattering Characteristics of Tiltrotor Aircraft Based on Dynamic Calculation Method
title_short Keen Investigation of the Electromagnetic Scattering Characteristics of Tiltrotor Aircraft Based on Dynamic Calculation Method
title_full Keen Investigation of the Electromagnetic Scattering Characteristics of Tiltrotor Aircraft Based on Dynamic Calculation Method
title_fullStr Keen Investigation of the Electromagnetic Scattering Characteristics of Tiltrotor Aircraft Based on Dynamic Calculation Method
title_full_unstemmed Keen Investigation of the Electromagnetic Scattering Characteristics of Tiltrotor Aircraft Based on Dynamic Calculation Method
title_sort keen investigation of the electromagnetic scattering characteristics of tiltrotor aircraft based on dynamic calculation method
publisher MDPI AG
series Photonics
issn 2304-6732
publishDate 2021-05-01
description To study the radar characteristics of the tiltrotor aircraft when considering rotor rotation and tilting actions, a dynamic calculation method (DCM) based on physical optics and physical theory of diffraction is presented. The results show that the radar cross section of a single rotor is dynamic and periodic when it rotates, while increasing the rotation speed can shorten this period. At a fixed tilt angle, the overall radar cross section of the cabin plus rotor still exhibits various dynamic characteristics at different azimuths when considering the rotation of the rotor. Increasing the tilt angle can better improve the electromagnetic scattering level of the rotor, but this easily makes the cabin and the outer end of the wing become a new source of strong scattering. In the heading direction, the dynamic radar cross section of the aircraft under a larger azimuth angle is lower when the cabin tilts from horizontal to vertical position. The presented DCM is feasible and effective to obtain the electromagnetic scattering characteristics of tiltrotor aircraft.
topic tiltrotor aircraft
radar stealth
dynamic electromagnetic scattering
radar cross-section
url https://www.mdpi.com/2304-6732/8/6/175
work_keys_str_mv AT zeyangzhou keeninvestigationoftheelectromagneticscatteringcharacteristicsoftiltrotoraircraftbasedondynamiccalculationmethod
AT junhuang keeninvestigationoftheelectromagneticscatteringcharacteristicsoftiltrotoraircraftbasedondynamiccalculationmethod
AT chenchen keeninvestigationoftheelectromagneticscatteringcharacteristicsoftiltrotoraircraftbasedondynamiccalculationmethod
AT jiarenzhang keeninvestigationoftheelectromagneticscatteringcharacteristicsoftiltrotoraircraftbasedondynamiccalculationmethod
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