NO870726L - Utskytningsanordning for et optisk ledet, traadstyrt missil med forbedrete elektroniske kretser. - Google Patents
Utskytningsanordning for et optisk ledet, traadstyrt missil med forbedrete elektroniske kretser.Info
- Publication number
- NO870726L NO870726L NO870726A NO870726A NO870726L NO 870726 L NO870726 L NO 870726L NO 870726 A NO870726 A NO 870726A NO 870726 A NO870726 A NO 870726A NO 870726 L NO870726 L NO 870726L
- Authority
- NO
- Norway
- Prior art keywords
- missile
- guided
- optically
- time
- launched
- Prior art date
Links
- 230000005484 gravity Effects 0.000 claims description 21
- 230000006870 function Effects 0.000 claims description 9
- 238000012546 transfer Methods 0.000 claims description 2
- 238000012937 correction Methods 0.000 description 7
- 238000010586 diagram Methods 0.000 description 5
- 230000009467 reduction Effects 0.000 description 5
- 230000003321 amplification Effects 0.000 description 3
- 238000003199 nucleic acid amplification method Methods 0.000 description 3
- 230000003287 optical effect Effects 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 2
- 238000013016 damping Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000018109 developmental process Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000010363 phase shift Effects 0.000 description 2
- NIOPZPCMRQGZCE-WEVVVXLNSA-N 2,4-dinitro-6-(octan-2-yl)phenyl (E)-but-2-enoate Chemical compound CCCCCCC(C)C1=CC([N+]([O-])=O)=CC([N+]([O-])=O)=C1OC(=O)\C=C\C NIOPZPCMRQGZCE-WEVVVXLNSA-N 0.000 description 1
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 239000000779 smoke Substances 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
Classifications
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| IL78757A IL78757A0 (en) | 1986-05-12 | 1986-05-12 | Launcher for an optically guided,wire-controlled missile with improved electronic circuitry |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| NO870726D0 NO870726D0 (no) | 1987-02-23 |
| NO870726L true NO870726L (no) | 1987-11-13 |
Family
ID=11056765
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NO870726A NO870726L (no) | 1986-05-12 | 1987-02-23 | Utskytningsanordning for et optisk ledet, traadstyrt missil med forbedrete elektroniske kretser. |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US4705237A (da) |
| EP (1) | EP0253919A3 (da) |
| DK (1) | DK90787A (da) |
| ES (1) | ES2012816A6 (da) |
| GR (1) | GR870293B (da) |
| IL (1) | IL78757A0 (da) |
| NO (1) | NO870726L (da) |
| PT (1) | PT84451B (da) |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5035375A (en) * | 1988-12-19 | 1991-07-30 | Hughes Aircraft Company | Fiber optic radar guided missile system |
| US5082199A (en) * | 1989-07-21 | 1992-01-21 | Hughes Aircraft Company | Digital electronics assembly for a tube-launched missile |
| US5123610A (en) * | 1989-07-21 | 1992-06-23 | Hughes Aircraft Company | Retrofit digital electronics unit for a tube-launched missile |
| US5080300A (en) * | 1989-12-07 | 1992-01-14 | Hughes Aircraft Company | Launcher control system for surface launched active radar missiles |
| US5118050A (en) * | 1989-12-07 | 1992-06-02 | Hughes Aircraft Company | Launcher control system |
| US5042742A (en) * | 1989-12-22 | 1991-08-27 | Hughes Aircraft Company | Microcontroller for controlling an airborne vehicle |
| US5074491A (en) * | 1990-08-14 | 1991-12-24 | Hughes Aircraft Company | Method for correcting misalignment between multiple missile track links |
| US5096139A (en) * | 1990-08-16 | 1992-03-17 | Hughes Aircraft Company | Missile interface unit |
| US5106033A (en) * | 1991-03-22 | 1992-04-21 | Hughes Aircraft Company | Missile guidance electronics assembly for portable guided missile launcher |
| US20050131592A1 (en) * | 2003-12-15 | 2005-06-16 | The Boeing Company | In-flight control system stability margin assessment |
| RU2261412C1 (ru) * | 2004-07-23 | 2005-09-27 | Государственное унитарное предприятие "Конструкторское бюро приборостроения" | Способ наведения управляемой ракеты и пусковая установка для его реализации |
| US10429151B2 (en) | 2017-06-13 | 2019-10-01 | Raytheon Company | Recapture of remotely-tracked command guided vehicle into the tracker's field-of-view |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| NL132546C (da) * | 1961-11-06 | |||
| US3366346A (en) * | 1965-07-19 | 1968-01-30 | Army Usa | Remote missile command system |
| US3711046A (en) * | 1969-10-22 | 1973-01-16 | H Barhydt | Automatic missile guidance system |
| SE364360B (da) * | 1972-06-26 | 1974-02-18 | Bofors Ab | |
| US4406429A (en) * | 1978-04-13 | 1983-09-27 | Texas Instruments Incorporated | Missile detecting and tracking unit |
| US4474343A (en) * | 1981-05-04 | 1984-10-02 | Hughes Aircraft Company | Jitter compensating scene stabilizing missile guidance system |
| GB2132794B (en) * | 1982-12-18 | 1986-02-26 | British Aerospace | Missile guidance system |
| 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 |
-
1986
- 1986-05-12 IL IL78757A patent/IL78757A0/xx unknown
- 1986-08-14 EP EP86111273A patent/EP0253919A3/en not_active Withdrawn
- 1986-10-16 US US06/919,666 patent/US4705237A/en not_active Expired - Fee Related
-
1987
- 1987-02-23 GR GR870293A patent/GR870293B/el unknown
- 1987-02-23 NO NO870726A patent/NO870726L/no unknown
- 1987-02-23 DK DK090787A patent/DK90787A/da not_active Application Discontinuation
- 1987-03-09 ES ES8700639A patent/ES2012816A6/es not_active Expired - Lifetime
- 1987-03-11 PT PT84451A patent/PT84451B/pt not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| NO870726D0 (no) | 1987-02-23 |
| PT84451A (en) | 1987-04-01 |
| GR870293B (en) | 1987-09-07 |
| EP0253919A3 (en) | 1989-04-26 |
| DK90787D0 (da) | 1987-02-23 |
| ES2012816A6 (es) | 1990-04-16 |
| EP0253919A2 (en) | 1988-01-27 |
| US4705237A (en) | 1987-11-10 |
| PT84451B (pt) | 1989-12-29 |
| DK90787A (da) | 1987-11-13 |
| IL78757A0 (en) | 1986-08-31 |
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