IL94760A - יחידת כלאים אלקטרונית לטיל המשוגר בעזרת קנה - Google Patents

יחידת כלאים אלקטרונית לטיל המשוגר בעזרת קנה

Info

Publication number
IL94760A
IL94760A IL9476090A IL9476090A IL94760A IL 94760 A IL94760 A IL 94760A IL 9476090 A IL9476090 A IL 9476090A IL 9476090 A IL9476090 A IL 9476090A IL 94760 A IL94760 A IL 94760A
Authority
IL
Israel
Prior art keywords
acc
signal
hsi
yaw
control signal
Prior art date
Application number
IL9476090A
Other languages
English (en)
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
Publication of IL94760A publication Critical patent/IL94760A/he

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • 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
    • F41G7/30—Command link guidance systems
    • F41G7/301—Details
    • 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
    • F41G7/30—Command link guidance systems
    • F41G7/32—Command link guidance systems for wire-guided missiles
IL9476090A 1989-07-21 1990-06-18 יחידת כלאים אלקטרונית לטיל המשוגר בעזרת קנה IL94760A (he)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/384,228 US5082199A (en) 1989-07-21 1989-07-21 Digital electronics assembly for a tube-launched missile

Publications (1)

Publication Number Publication Date
IL94760A true IL94760A (he) 1995-12-08

Family

ID=23516514

Family Applications (2)

Application Number Title Priority Date Filing Date
IL9476090A IL94760A (he) 1989-07-21 1990-06-18 יחידת כלאים אלקטרונית לטיל המשוגר בעזרת קנה
IL94759A IL94759A0 (en) 1989-07-21 1990-06-18 Retrofit digital electronics unit for a tube-launched missile

Family Applications After (1)

Application Number Title Priority Date Filing Date
IL94759A IL94759A0 (en) 1989-07-21 1990-06-18 Retrofit digital electronics unit for a tube-launched missile

Country Status (10)

Country Link
US (1) US5082199A (he)
EP (1) EP0412654B1 (he)
JP (1) JP2542109B2 (he)
KR (1) KR940004648B1 (he)
AU (1) AU630476B2 (he)
CA (1) CA2018814C (he)
DE (1) DE69022336T2 (he)
ES (1) ES2088972T3 (he)
IL (2) IL94760A (he)
NO (1) NO180557C (he)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5123610A (en) * 1989-07-21 1992-06-23 Hughes Aircraft Company Retrofit digital electronics unit for a tube-launched missile

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4037202A (en) * 1975-04-21 1977-07-19 Raytheon Company Microprogram controlled digital processor having addressable flip/flop section
US4185796A (en) * 1976-12-13 1980-01-29 The United States Of America As Represented By The Secretary Of The Army Fiber optic missile guidance and control
JPS5866120A (ja) * 1981-10-16 1983-04-20 Nissan Motor Co Ltd 飛翔体の姿勢制御装置
US4611771A (en) * 1985-04-18 1986-09-16 United States Of America As Represented By The Secretary Of The Army Fiber optic track/reaim system
US4662580A (en) * 1985-06-20 1987-05-05 The United States Of America As Represented By The Secretary Of The Navy Simple diver reentry method
IL78757A0 (en) * 1986-05-12 1986-08-31 Israel State Launcher for an optically guided,wire-controlled missile with improved electronic circuitry
US4732349A (en) * 1986-10-08 1988-03-22 Hughes Aircraft Company Beamrider guidance system
US4770370A (en) * 1987-03-31 1988-09-13 The Boeing Company Optical fiber guided tube-launched projectile system
US4899956A (en) * 1988-07-20 1990-02-13 Teleflex, Incorporated Self-contained supplemental guidance module for projectile weapons
US5123610A (en) * 1989-07-21 1992-06-23 Hughes Aircraft Company Retrofit digital electronics unit for a tube-launched missile

Also Published As

Publication number Publication date
KR910003354A (ko) 1991-02-27
DE69022336T2 (de) 1996-03-28
CA2018814C (en) 1994-04-19
AU630476B2 (en) 1992-10-29
CA2018814A1 (en) 1991-01-21
NO180557B (no) 1997-01-27
US5082199A (en) 1992-01-21
NO180557C (no) 1997-05-07
EP0412654B1 (en) 1995-09-13
AU5918190A (en) 1991-01-24
JPH0375500A (ja) 1991-03-29
KR940004648B1 (ko) 1994-05-27
DE69022336D1 (de) 1995-10-19
IL94759A0 (en) 1991-04-15
ES2088972T3 (es) 1996-10-01
EP0412654A1 (en) 1991-02-13
JP2542109B2 (ja) 1996-10-09
NO903099D0 (no) 1990-07-11
NO903099L (no) 1991-01-22

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Legal Events

Date Code Title Description
CE Application withdrawn (oppos. filed against grant of patent)

Free format text: APPLICANT WITHDREW APPLICATION ON 22.5.96