ES2081904T3 - Sistema de guia para misiles de peso ligero. - Google Patents

Sistema de guia para misiles de peso ligero.

Info

Publication number
ES2081904T3
ES2081904T3 ES90125482T ES90125482T ES2081904T3 ES 2081904 T3 ES2081904 T3 ES 2081904T3 ES 90125482 T ES90125482 T ES 90125482T ES 90125482 T ES90125482 T ES 90125482T ES 2081904 T3 ES2081904 T3 ES 2081904T3
Authority
ES
Spain
Prior art keywords
missile
angle
sight line
line
projectile
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
ES90125482T
Other languages
English (en)
Inventor
Norman E Beam
Leonard D Vance
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.)
Raytheon Co
Original Assignee
Hughes Aircraft Co
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 Aircraft Co filed Critical Hughes Aircraft Co
Application granted granted Critical
Publication of ES2081904T3 publication Critical patent/ES2081904T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/02—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by astronomical means
    • G01C21/025—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by astronomical means with the use of startrackers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2253—Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2273—Homing guidance systems characterised by the type of waves
    • F41G7/2293—Homing guidance systems characterised by the type of waves using electromagnetic waves other than radio waves
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/12—Target-seeking control

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • General Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • Electromagnetism (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Navigation (AREA)
  • Details Of Aerials (AREA)

Abstract

SE PRESENTA UN SISTEMA DE CONTROL DE MISILES DE POCO PESO (14) QUE CONSTA DE UN PROYECTIL BUSCADOR (16) QUE PROPORCIONA UNA PRIMERA SEÑAL INDICADORA DE UN ANGULO (PERTENECE A) ENTRE UNA LINEA DE MIRA (15) DEL MISIL (10) A UN BLANCO (12) Y UN EJE LONGITUDINAL (9) QUE SE EXTIENDE A TRAVES DEL MISIL (10). EL PROYECTIL BUSCADOR (16) PROPORCIONA TAMBIEN UNA SEGUNDA SEÑAL INDICADORA DE UN SEGUNDO ANGULO (DELTA) ENTRE EL EJE LONGITUDINAL (9) QUE SE EXTIENDE A TRAVES DEL MISIL (10) Y UNA LINEA DEMIRA (11) ENTRE EL MISIL (10) Y UN CUERPO CELESTE (13). SE INCLUYE UN PROCESADOR (18) PARA COMPUTERIZAR EL ANGULO DE LA LINEA DE MIRA (SIGMA) ENTRE LA LINEA DE MIRA (15) DEL MISIL (10) AL BLANCO (12) Y LA LINEA DE MIRA (11) DEL MISIL (10) AL CUERPO CELESTE (13) DESDE LOS ANGULOS PRIMERO Y SEGUNDO (PERTENECE A) Y (DELTA). UN SUBSISTEMA DE CONTROL TERMINAL (24) COMPUTIZA LOS COMANDOS DE ACELERACION DESDE EL ANGULO (SIGMA) DE LA LINEA DE MIRA QUE SE UTILIZAN, MEDIANTE UN SISTEMA DE PROPULSION (26), PARA CAMBIAR LA VELOCIDAD DEL MISIL (10) EN RESPUESTA AL MISMO.
ES90125482T 1990-01-08 1990-12-24 Sistema de guia para misiles de peso ligero. Expired - Lifetime ES2081904T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/462,181 US5022608A (en) 1990-01-08 1990-01-08 Lightweight missile guidance system

Publications (1)

Publication Number Publication Date
ES2081904T3 true ES2081904T3 (es) 1996-03-16

Family

ID=23835467

Family Applications (1)

Application Number Title Priority Date Filing Date
ES90125482T Expired - Lifetime ES2081904T3 (es) 1990-01-08 1990-12-24 Sistema de guia para misiles de peso ligero.

Country Status (10)

Country Link
US (1) US5022608A (es)
EP (1) EP0436215B1 (es)
JP (1) JP2638686B2 (es)
KR (1) KR940004647B1 (es)
AU (1) AU617063B2 (es)
CA (1) CA2032267C (es)
DE (1) DE69025049T2 (es)
ES (1) ES2081904T3 (es)
IL (1) IL96671A (es)
NO (1) NO300189B1 (es)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5681009A (en) * 1996-09-27 1997-10-28 Lockheed Missiles And Space Company Missile having endoatmospheric and exoatmospheric seeker capability
US6494140B1 (en) 1999-04-22 2002-12-17 Lockheed Martin Corporation Modular rocket boosted penetrating warhead
US6276277B1 (en) 1999-04-22 2001-08-21 Lockheed Martin Corporation Rocket-boosted guided hard target penetrator
US7007888B2 (en) * 2003-11-25 2006-03-07 The Boeing Company Inertial position target measuring systems and methods
IL162863A (en) * 2004-07-05 2012-08-30 Israel Aerospace Ind Ltd Exo atmospheric intercepting system and method
US20060235614A1 (en) * 2005-04-14 2006-10-19 Starvision Technologies Inc. Method and Apparatus for Automatic Identification of Celestial Bodies
US8222582B1 (en) * 2008-09-30 2012-07-17 Anderson Mark J Celestial navigation using stellar narrow-band emission
WO2011002343A1 (en) * 2009-06-30 2011-01-06 Saab Ab An extended method for terminal guidance
US8735788B2 (en) * 2011-02-18 2014-05-27 Raytheon Company Propulsion and maneuvering system with axial thrusters and method for axial divert attitude and control
CN111351401B (zh) * 2018-12-21 2022-12-23 北京理工大学 应用于捷联导引头制导飞行器的防侧偏制导方法
CN110926278B (zh) * 2019-12-04 2021-12-31 中国人民解放军海军潜艇学院 一种采用多前置角叠加与末端修正的前置导引方法
CN111102886B (zh) * 2019-12-12 2022-03-25 中国人民解放军海军航空大学 一种小微飞行器无陀螺精确制导方法
CN111366044B (zh) * 2019-12-29 2022-10-04 湖北航天飞行器研究所 一种平飞过渡段制导控制方法

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3025023A (en) * 1954-09-14 1962-03-13 John W B Barghausen Missile guidance system
US3499156A (en) * 1966-02-16 1970-03-03 Goodyear Aerospace Corp Celestial matching system for attitude stabilization and position determination
GB1600201A (en) * 1967-09-11 1981-10-14 British Aerospace Guidance systems
SE430102B (sv) * 1981-10-08 1983-10-17 Saab Scania Ab Sett och anordning for styrning av en aerodynamisk kropp med skrovfast malsokare
JPS6052504U (ja) * 1983-09-12 1985-04-13 三菱電機株式会社 飛しよう体シ−カヘツドセンサ駆動サ−ボ装置
JPS6123222A (ja) * 1984-07-10 1986-01-31 Nec Corp 誘導方式
JPS62125895U (es) * 1986-01-27 1987-08-10

Also Published As

Publication number Publication date
CA2032267A1 (en) 1991-07-09
NO905476L (no) 1991-07-02
US5022608A (en) 1991-06-11
DE69025049D1 (de) 1996-03-07
DE69025049T2 (de) 1996-05-30
JP2638686B2 (ja) 1997-08-06
IL96671A0 (en) 1992-05-25
JPH04110600A (ja) 1992-04-13
NO300189B1 (no) 1997-04-21
NO905476D0 (no) 1990-12-19
KR940004647B1 (ko) 1994-05-27
EP0436215A2 (en) 1991-07-10
EP0436215A3 (en) 1992-10-28
CA2032267C (en) 1994-04-19
IL96671A (en) 1993-08-18
AU6820090A (en) 1991-07-18
EP0436215B1 (en) 1996-01-24
AU617063B2 (en) 1991-11-14
KR910014678A (ko) 1991-08-31

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