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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Editorial Office of Aero Weaponry
2021
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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) |
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|navigation|doppler test|guidance radar|velocity correction|velocity measurement Motor vehicles. Aeronautics. Astronautics TL1-4050 |
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|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 |
work_keys_str_mv |
AT zhaoyihuanyinjianyongyanghongqiaochenweiliaohuashan aschemeofgroundvelocitymeasurementassistedbymissileborneradar AT zhaoyihuanyinjianyongyanghongqiaochenweiliaohuashan schemeofgroundvelocitymeasurementassistedbymissileborneradar |
_version_ |
1718406860904595456 |