A Scheme of Ground Velocity Measurement Assisted by Missile-Borne Radar

In order to solve the problem of precise navigation of long endurance missile when satellite signal is unavailable, an integrated scheme for ground velocity measurement of carrier by using missile-borne guidance radar is proposed. The calculation methods of three-dimensional ground velocity measurem...

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Autor principal: Zhao Yihuan, Yin Jianyong, Yang Hongqiao, Chen Wei, Liao Huashan
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Lenguaje:ZH
Publicado: Editorial Office of Aero Weaponry 2021
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Acceso en línea:https://doaj.org/article/4864abe48aee464ba439567a2afaaf78
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spelling oai:doaj.org-article:4864abe48aee464ba439567a2afaaf782021-11-30T00:13:41ZA Scheme of Ground Velocity Measurement Assisted by Missile-Borne Radar1673-504810.12132/ISSN.1673-5048.2020.0140https://doaj.org/article/4864abe48aee464ba439567a2afaaf782021-06-01T00:00:00Zhttps://www.aeroweaponry.avic.com/fileup/1673-5048/PDF/1628469451528-739359674.pdfhttps://doaj.org/toc/1673-5048In order to solve the problem of precise navigation of long endurance missile when satellite signal is unavailable, an integrated scheme for ground velocity measurement of carrier by using missile-borne guidance radar is proposed. The calculation methods of three-dimensional ground velocity measurement with "X" and "T" antenna layout are deduced. The antenna beam parameters, waveform parameters, RF components and signal processing architecture are designed. The measurement error of the system is analyzed. The results show that the auxiliary measurement of carrier ground velocity can meet the needs of carrier navigation velocity correction and improve the equipment integration.Zhao Yihuan, Yin Jianyong, Yang Hongqiao, Chen Wei, Liao HuashanEditorial Office of Aero Weaponryarticle|navigation|doppler test|guidance radar|velocity correction|velocity measurementMotor vehicles. Aeronautics. AstronauticsTL1-4050ZHHangkong bingqi, Vol 28, Iss 3, Pp 65-70 (2021)
institution DOAJ
collection DOAJ
language ZH
topic |navigation|doppler test|guidance radar|velocity correction|velocity measurement
Motor vehicles. Aeronautics. Astronautics
TL1-4050
spellingShingle |navigation|doppler test|guidance radar|velocity correction|velocity measurement
Motor vehicles. Aeronautics. Astronautics
TL1-4050
Zhao Yihuan, Yin Jianyong, Yang Hongqiao, Chen Wei, Liao Huashan
A Scheme of Ground Velocity Measurement Assisted by Missile-Borne Radar
description In order to solve the problem of precise navigation of long endurance missile when satellite signal is unavailable, an integrated scheme for ground velocity measurement of carrier by using missile-borne guidance radar is proposed. The calculation methods of three-dimensional ground velocity measurement with "X" and "T" antenna layout are deduced. The antenna beam parameters, waveform parameters, RF components and signal processing architecture are designed. The measurement error of the system is analyzed. The results show that the auxiliary measurement of carrier ground velocity can meet the needs of carrier navigation velocity correction and improve the equipment integration.
format article
author Zhao Yihuan, Yin Jianyong, Yang Hongqiao, Chen Wei, Liao Huashan
author_facet Zhao Yihuan, Yin Jianyong, Yang Hongqiao, Chen Wei, Liao Huashan
author_sort Zhao Yihuan, Yin Jianyong, Yang Hongqiao, Chen Wei, Liao Huashan
title A Scheme of Ground Velocity Measurement Assisted by Missile-Borne Radar
title_short A Scheme of Ground Velocity Measurement Assisted by Missile-Borne Radar
title_full A Scheme of Ground Velocity Measurement Assisted by Missile-Borne Radar
title_fullStr A Scheme of Ground Velocity Measurement Assisted by Missile-Borne Radar
title_full_unstemmed A Scheme of Ground Velocity Measurement Assisted by Missile-Borne Radar
title_sort scheme of ground velocity measurement assisted by missile-borne radar
publisher Editorial Office of Aero Weaponry
publishDate 2021
url https://doaj.org/article/4864abe48aee464ba439567a2afaaf78
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