ES2189338T3 - Configuracion de antena para satelites en orbita terrestre baja y media. - Google Patents

Configuracion de antena para satelites en orbita terrestre baja y media.

Info

Publication number
ES2189338T3
ES2189338T3 ES99123001T ES99123001T ES2189338T3 ES 2189338 T3 ES2189338 T3 ES 2189338T3 ES 99123001 T ES99123001 T ES 99123001T ES 99123001 T ES99123001 T ES 99123001T ES 2189338 T3 ES2189338 T3 ES 2189338T3
Authority
ES
Spain
Prior art keywords
lens
antenna configuration
variety
satellites
medium
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
ES99123001T
Other languages
English (en)
Inventor
Sudhakar Rao
Philip H Law
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
DirecTV Group Inc
Original Assignee
Hughes Electronics Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hughes Electronics Corp filed Critical Hughes Electronics Corp
Application granted granted Critical
Publication of ES2189338T3 publication Critical patent/ES2189338T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • H01Q3/26—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture
    • H01Q3/2605—Array of radiating elements provided with a feedback control over the element weights, e.g. adaptive arrays
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q19/00—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
    • H01Q19/06—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using refracting or diffracting devices, e.g. lens
    • H01Q19/08—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using refracting or diffracting devices, e.g. lens for modifying the radiation pattern of a radiating horn in which it is located

Landscapes

  • Aerials With Secondary Devices (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

Una configuración de antena adecuada para satélites LEO/MEO incluye una variedad de lentes (32) donde cada lente tiene una variedad de antenas de alimentación (42) ubicadas con respecto a la lente (32). La lente (32) tiene una primera superficie (40) y una segunda superficie (38). La variedad de antenas de alimentación (42) se disponen en una superficie curva (44). Cada una de las diversas antenas de alimentación (42) genera un rayo (22) que tiene una distribución de fase. Las distribuciones de fase tienen una relación de fase predeterminada con una primera superficie (40) y preferentemente la segunda superficie (38). Esto permite a la lente (32) transmitir y recibir una señal con una distribución de fase deseada a través de una sección transversal del rayo. Las rayos de las diversas lentes (32) se entrelazan en el suelo para formar un recubrimiento contiguo con múltiples puntos de rayo que se solapan.
ES99123001T 1998-11-20 1999-11-19 Configuracion de antena para satelites en orbita terrestre baja y media. Expired - Lifetime ES2189338T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/196,864 US6184838B1 (en) 1998-11-20 1998-11-20 Antenna configuration for low and medium earth orbit satellites

Publications (1)

Publication Number Publication Date
ES2189338T3 true ES2189338T3 (es) 2003-07-01

Family

ID=22727082

Family Applications (1)

Application Number Title Priority Date Filing Date
ES99123001T Expired - Lifetime ES2189338T3 (es) 1998-11-20 1999-11-19 Configuracion de antena para satelites en orbita terrestre baja y media.

Country Status (4)

Country Link
US (2) US6184838B1 (es)
EP (1) EP1003241B1 (es)
DE (1) DE69905540T2 (es)
ES (1) ES2189338T3 (es)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10205379A1 (de) * 2002-02-09 2003-08-21 Bosch Gmbh Robert Vorrichtung zum Senden und Empfangen elektromagnetischer Strahlung
JP2004158911A (ja) 2002-11-01 2004-06-03 Murata Mfg Co Ltd セクタアンテナ装置および車載用送受信装置
US6961025B1 (en) * 2003-08-18 2005-11-01 Lockheed Martin Corporation High-gain conformal array antenna
US7193574B2 (en) * 2004-10-18 2007-03-20 Interdigital Technology Corporation Antenna for controlling a beam direction both in azimuth and elevation
WO2006130725A2 (en) * 2005-05-31 2006-12-07 Interdigital Technology Corporation Authentication and encryption methods using shared secret randomness in a joint channel
WO2009100153A1 (en) * 2008-02-05 2009-08-13 Ems Technologies, Inc. Modal beam positioning
US8249306B2 (en) 2008-03-18 2012-08-21 Certusview Technologies, Llc Virtual white lines for delimiting planned excavation sites
US10135137B2 (en) 2015-02-20 2018-11-20 Northrop Grumman Systems Corporation Low cost space-fed reconfigurable phased array for spacecraft and aircraft applications
EP3500873A4 (en) * 2016-08-20 2020-08-12 Astrome Technologies Private Limited SYSTEM AND PROCESS FOR THE INTEGRATED OPTIMIZATION OF DESIGN AND PERFORMANCE OF SATELLITE CONSTELLATIONS
CN112164885B (zh) * 2020-08-24 2022-10-14 西安空间无线电技术研究所 一种基于多馈源合成网络的幅相优化设计方法
CN112422170B (zh) * 2020-11-09 2022-10-28 大连交通大学 双频段射频设备近场自动化检测方法
CN112526512B (zh) * 2020-11-23 2022-07-22 电子科技大学 大功率大口径宽带毫米波空馈相控阵雷达系统及成像方法
USD1026428S1 (en) * 2021-11-10 2024-05-14 Puma SE Shoe

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3835469A (en) * 1972-11-02 1974-09-10 Hughes Aircraft Co Optical limited scan antenna system
DE2738549A1 (de) 1977-08-26 1979-03-01 Licentia Gmbh Mikrowellen-antenne
US5099253A (en) 1989-11-06 1992-03-24 Raytheon Company Constant beamwidth scanning array
FR2679704B1 (fr) * 1991-07-26 1993-09-24 Alcatel Espace Antenne-reseau pour ondes hyperfrequences.
EP0707356A1 (en) 1994-04-28 1996-04-17 Tovarischestvo S Ogranichennoi Otvetsvennostju "Konkur" Multiple beam lens antenna
US5821908A (en) * 1996-03-22 1998-10-13 Ball Aerospace And Technologies Corp. Spherical lens antenna having an electronically steerable beam
FR2762936B1 (fr) 1997-04-30 1999-06-11 Alsthom Cge Alcatel Dispositif terminal-antenne pour constellation de satellites defilants

Also Published As

Publication number Publication date
EP1003241A1 (en) 2000-05-24
US6184838B1 (en) 2001-02-06
DE69905540T2 (de) 2003-12-18
US6323815B1 (en) 2001-11-27
EP1003241B1 (en) 2003-02-26
DE69905540D1 (de) 2003-04-03

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