CN113272671B - 使用具有不同开度角的两个天线的飞行器制导 - Google Patents

使用具有不同开度角的两个天线的飞行器制导 Download PDF

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Publication number
CN113272671B
CN113272671B CN201980074200.2A CN201980074200A CN113272671B CN 113272671 B CN113272671 B CN 113272671B CN 201980074200 A CN201980074200 A CN 201980074200A CN 113272671 B CN113272671 B CN 113272671B
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CN
China
Prior art keywords
antenna
power
aircraft
deviation
guidance system
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CN201980074200.2A
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English (en)
Chinese (zh)
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CN113272671A (zh
Inventor
西尔万·伯伊拉德
阿兰·乔帝尼
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Safran Electronics and Defense SAS
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Safran Electronics and Defense SAS
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Publication of CN113272671A publication Critical patent/CN113272671A/zh
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Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S3/00—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
    • G01S3/02—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using radio waves
    • G01S3/14—Systems for determining direction or deviation from predetermined direction
    • G01S3/28—Systems for determining direction or deviation from predetermined direction using amplitude comparison of signals derived simultaneously from receiving antennas or antenna systems having differently-oriented directivity characteristics
    • G01S3/30—Systems for determining direction or deviation from predetermined direction using amplitude comparison of signals derived simultaneously from receiving antennas or antenna systems having differently-oriented directivity characteristics derived directly from separate directional systems
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S3/00—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
    • G01S3/02—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using radio waves
    • G01S3/14—Systems for determining direction or deviation from predetermined direction
    • G01S3/28—Systems for determining direction or deviation from predetermined direction using amplitude comparison of signals derived simultaneously from receiving antennas or antenna systems having differently-oriented directivity characteristics
    • G01S3/32—Systems for determining direction or deviation from predetermined direction using amplitude comparison of signals derived simultaneously from receiving antennas or antenna systems having differently-oriented directivity characteristics derived from different combinations of signals from separate antennas, e.g. comparing sum with difference
    • G01S3/34—Systems for determining direction or deviation from predetermined direction using amplitude comparison of signals derived simultaneously from receiving antennas or antenna systems having differently-oriented directivity characteristics derived from different combinations of signals from separate antennas, e.g. comparing sum with difference the separate antennas comprising one directional antenna and one non-directional antenna, e.g. combination of loop and open antennas producing a reversed cardioid directivity characteristic
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/02—Control of position or course in two dimensions
    • G05D1/0202—Control of position or course in two dimensions specially adapted to aircraft
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q25/00—Antennas or antenna systems providing at least two radiating patterns
    • H01Q25/002—Antennas or antenna systems providing at least two radiating patterns providing at least two patterns of different beamwidth; Variable beamwidth antennas
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/02—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/02—Automatic approach or landing aids, i.e. systems in which flight data of incoming planes are processed to provide landing data
    • G08G5/025—Navigation or guidance aids
CN201980074200.2A 2018-09-27 2019-09-27 使用具有不同开度角的两个天线的飞行器制导 Active CN113272671B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1801007A FR3086784B1 (fr) 2018-09-27 2018-09-27 Guidage d'un aeronef a l'aide de deux antennes presentant un angle d'ouverture different
FR1801007 2018-09-27
PCT/EP2019/076320 WO2020065074A1 (fr) 2018-09-27 2019-09-27 Guidage d'un aéronef à l'aide de deux antennes présentant un angle d'ouverture différent

Publications (2)

Publication Number Publication Date
CN113272671A CN113272671A (zh) 2021-08-17
CN113272671B true CN113272671B (zh) 2023-12-22

Family

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Family Applications (1)

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CN201980074200.2A Active CN113272671B (zh) 2018-09-27 2019-09-27 使用具有不同开度角的两个天线的飞行器制导

Country Status (5)

Country Link
EP (1) EP3857249A1 (fr)
CN (1) CN113272671B (fr)
FR (1) FR3086784B1 (fr)
IL (1) IL281831A (fr)
WO (1) WO2020065074A1 (fr)

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US4136343A (en) * 1977-05-02 1979-01-23 Martin Marietta Corporation Multiple source tracking system
CN1306710A (zh) * 1997-12-16 2001-08-01 北点技术有限公司 对于地面广播信号再使用卫星广播频谱的设备和方法
JP2010181074A (ja) * 2009-02-04 2010-08-19 Toshiba Corp 誘導装置
CN103454647A (zh) * 2012-06-01 2013-12-18 霍尼韦尔国际公司 用于对飞行器导航系统中的天线的选择的系统和方法
CN104319483A (zh) * 2014-10-16 2015-01-28 中国科学院深圳先进技术研究院 一种可调控的天线系统及天线的调控方法
CN105144472A (zh) * 2013-04-02 2015-12-09 瑞典爱立信有限公司 无线电天线定位
CN105186102A (zh) * 2015-09-15 2015-12-23 西安星通通信科技有限公司 基于数字波束跟踪的动中通天线系统及跟踪方法
US9304198B1 (en) * 2013-10-04 2016-04-05 Sandia Corporation Navigator alignment using radar scan
CN106415672A (zh) * 2014-03-31 2017-02-15 赛峰电子与防务公司 通过在检测到飞行器的紧急状况时其方向性发生变化的无线电波束对飞行器的黑匣子所记录的飞行数据进行传输的方法
CN107407937A (zh) * 2015-03-16 2017-11-28 赛峰电子与防务公司 航空器着陆的自动辅助方法
CN108293094A (zh) * 2016-02-29 2018-07-17 惠普发展公司有限责任合伙企业 使用单向和全向天线确定物体图像是否在相机取景器中

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US6417803B1 (en) * 2001-04-03 2002-07-09 The Boeing Company Beam alignment system and method for an antenna
US7313403B2 (en) * 2003-08-06 2007-12-25 Hong Kong Applied Science And Technology Research Institute Co., Ltd. Location positioning in wireless networks
CN101652942A (zh) * 2007-03-15 2010-02-17 罗盘自动跟踪器有限责任公司 用于测向仪的设备和方法
US9885777B2 (en) * 2014-01-10 2018-02-06 Raytheon Company Detection of stealth vehicles using VHF radar
US10135126B2 (en) * 2015-06-05 2018-11-20 Viasat, Inc. Methods and systems for mitigating interference with a nearby satellite
US10211530B2 (en) * 2016-07-01 2019-02-19 Gogo Llc Dynamic effective radiated power (ERP) adjustment

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US4136343A (en) * 1977-05-02 1979-01-23 Martin Marietta Corporation Multiple source tracking system
CN1306710A (zh) * 1997-12-16 2001-08-01 北点技术有限公司 对于地面广播信号再使用卫星广播频谱的设备和方法
JP2010181074A (ja) * 2009-02-04 2010-08-19 Toshiba Corp 誘導装置
CN103454647A (zh) * 2012-06-01 2013-12-18 霍尼韦尔国际公司 用于对飞行器导航系统中的天线的选择的系统和方法
CN105144472A (zh) * 2013-04-02 2015-12-09 瑞典爱立信有限公司 无线电天线定位
US9304198B1 (en) * 2013-10-04 2016-04-05 Sandia Corporation Navigator alignment using radar scan
CN106415672A (zh) * 2014-03-31 2017-02-15 赛峰电子与防务公司 通过在检测到飞行器的紧急状况时其方向性发生变化的无线电波束对飞行器的黑匣子所记录的飞行数据进行传输的方法
CN104319483A (zh) * 2014-10-16 2015-01-28 中国科学院深圳先进技术研究院 一种可调控的天线系统及天线的调控方法
CN107407937A (zh) * 2015-03-16 2017-11-28 赛峰电子与防务公司 航空器着陆的自动辅助方法
CN105186102A (zh) * 2015-09-15 2015-12-23 西安星通通信科技有限公司 基于数字波束跟踪的动中通天线系统及跟踪方法
CN108293094A (zh) * 2016-02-29 2018-07-17 惠普发展公司有限责任合伙企业 使用单向和全向天线确定物体图像是否在相机取景器中

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Analysis of Phased Array Antennas Vibration Effects on the Performance of Shipborne MLS;Xie Hongsen et al.;Applied Mechanics and Materials;全文 *
利用GNSS实现高轨卫星自主导航的新方案;何清举;孙前贵;;飞行器测控学报(第01期);全文 *
基于北斗双模终端的散射天线对准系统;王立国;叶亮;;无线电工程(第05期);全文 *
对再入飞行器精确制导的探讨;郭鹏鹏 等;企业技术开发;第34卷(第32期);全文 *
弹载主INS与SAR天线IMU传递对准方法;孟京;哈尔滨工业大学学报;第44卷(第1期);全文 *

Also Published As

Publication number Publication date
WO2020065074A1 (fr) 2020-04-02
IL281831A (en) 2021-05-31
FR3086784A1 (fr) 2020-04-03
FR3086784B1 (fr) 2020-09-25
EP3857249A1 (fr) 2021-08-04
CN113272671A (zh) 2021-08-17

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