NO301140B1 - Hybrid, analog/digital elektronisk styreenhet for et rörutskutt missil - Google Patents
Hybrid, analog/digital elektronisk styreenhet for et rörutskutt missil Download PDFInfo
- Publication number
- NO301140B1 NO301140B1 NO903100A NO903100A NO301140B1 NO 301140 B1 NO301140 B1 NO 301140B1 NO 903100 A NO903100 A NO 903100A NO 903100 A NO903100 A NO 903100A NO 301140 B1 NO301140 B1 NO 301140B1
- Authority
- NO
- Norway
- Prior art keywords
- signal
- yaw
- control signal
- missile
- pitch
- Prior art date
Links
- 230000033001 locomotion Effects 0.000 claims description 13
- 238000006243 chemical reaction Methods 0.000 claims 1
- 230000007246 mechanism Effects 0.000 description 18
- 239000012190 activator Substances 0.000 description 16
- 238000010586 diagram Methods 0.000 description 7
- 229910000831 Steel Inorganic materials 0.000 description 3
- 210000004556 brain Anatomy 0.000 description 3
- 239000000835 fiber Substances 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 238000004904 shortening Methods 0.000 description 2
- 230000006641 stabilisation Effects 0.000 description 2
- 238000011105 stabilization Methods 0.000 description 2
- 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
- 241000273930 Brevoortia tyrannus Species 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 230000001404 mediated effect Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 239000000523 sample Substances 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 230000008054 signal transmission Effects 0.000 description 1
- 230000000007 visual effect Effects 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
- F41G7/301—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
-
- 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
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/107—Simultaneous control of position or course in three dimensions specially adapted for missiles
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (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 |
|---|---|---|---|
| US07/384,229 US5123610A (en) | 1989-07-21 | 1989-07-21 | Retrofit digital electronics unit for a tube-launched missile |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| NO903100D0 NO903100D0 (no) | 1990-07-11 |
| NO903100L NO903100L (no) | 1991-01-22 |
| NO301140B1 true NO301140B1 (no) | 1997-09-15 |
Family
ID=23516518
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NO903100A NO301140B1 (no) | 1989-07-21 | 1990-07-11 | Hybrid, analog/digital elektronisk styreenhet for et rörutskutt missil |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US5123610A (ko) |
| EP (1) | EP0409614B1 (ko) |
| JP (1) | JP2541693B2 (ko) |
| KR (1) | KR940004646B1 (ko) |
| AU (1) | AU630211B2 (ko) |
| CA (1) | CA2018813C (ko) |
| DE (1) | DE69026317T2 (ko) |
| NO (1) | NO301140B1 (ko) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7474944B2 (en) * | 2002-10-22 | 2009-01-06 | The Boeing Company | Control system and method with multiple linked inputs |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5082199A (en) * | 1989-07-21 | 1992-01-21 | Hughes Aircraft Company | Digital electronics assembly for a tube-launched missile |
| FR2694390B1 (fr) * | 1992-07-28 | 1994-09-16 | Thomson Csf | Procédé de commande d'un missile minimisant sa distance de passage par rapport à une cible agile, et dispositif de mise en Óoeuvre. |
| DE4234878C2 (de) * | 1992-10-16 | 1995-03-30 | Deutsche Aerospace | Verfahren zur autonomen Lagesteuerung von Lenkflugkörpern |
| FR2748586B1 (fr) * | 1996-05-13 | 1998-07-17 | Aerospatiale | Dispositif de guidage d'un missile |
| US7343232B2 (en) | 2003-06-20 | 2008-03-11 | Geneva Aerospace | Vehicle control system including related methods and components |
| US7818127B1 (en) | 2004-06-18 | 2010-10-19 | Geneva Aerospace, Inc. | Collision avoidance for vehicle control systems |
| IL178840A0 (en) * | 2006-10-24 | 2007-09-20 | Rafael Advanced Defense Sys | System |
| CN106379559B (zh) * | 2016-09-29 | 2019-08-20 | 湖北航天技术研究院总体设计所 | 一种适用于导弹机载发射的过渡导航方法 |
| KR102061497B1 (ko) | 2019-05-31 | 2020-02-11 | (주)베셀 | 내진 기능을 갖는 물탱크 지지장치 |
| CN110304270B (zh) * | 2019-06-03 | 2021-01-05 | 宁波天擎航天科技有限公司 | 用于运载火箭的全方位发射控制方法、装置、计算机设备 |
Family Cites Families (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3008668A (en) * | 1955-06-06 | 1961-11-14 | Bell Telephone Labor Inc | Guidance control system |
| US3808542A (en) * | 1972-09-05 | 1974-04-30 | Singer Co | Pulse duration modulated to digital and analog converter for use in a gyro pickoff |
| US3900843A (en) * | 1972-09-05 | 1975-08-19 | Singer Co | Gyro pickoff apparatus to sense deviations of a vehicle axis from a gyro spin axis |
| 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 |
| 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 |
| US5082199A (en) * | 1989-07-21 | 1992-01-21 | Hughes Aircraft Company | Digital electronics assembly for a tube-launched missile |
-
1989
- 1989-07-21 US US07/384,229 patent/US5123610A/en not_active Expired - Lifetime
-
1990
- 1990-06-12 CA CA002018813A patent/CA2018813C/en not_active Expired - Fee Related
- 1990-07-11 NO NO903100A patent/NO301140B1/no not_active IP Right Cessation
- 1990-07-19 DE DE69026317T patent/DE69026317T2/de not_active Expired - Fee Related
- 1990-07-19 EP EP90307897A patent/EP0409614B1/en not_active Expired - Lifetime
- 1990-07-20 KR KR1019900011091A patent/KR940004646B1/ko not_active IP Right Cessation
- 1990-07-20 AU AU59180/90A patent/AU630211B2/en not_active Ceased
- 1990-07-20 JP JP2190944A patent/JP2541693B2/ja not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7474944B2 (en) * | 2002-10-22 | 2009-01-06 | The Boeing Company | Control system and method with multiple linked inputs |
Also Published As
| Publication number | Publication date |
|---|---|
| NO903100L (no) | 1991-01-22 |
| KR940004646B1 (ko) | 1994-05-27 |
| KR910003355A (ko) | 1991-02-27 |
| JPH03137500A (ja) | 1991-06-12 |
| CA2018813C (en) | 1995-01-03 |
| AU5918090A (en) | 1991-01-24 |
| EP0409614A3 (en) | 1992-06-03 |
| CA2018813A1 (en) | 1991-01-21 |
| DE69026317T2 (de) | 1996-11-21 |
| US5123610A (en) | 1992-06-23 |
| EP0409614A2 (en) | 1991-01-23 |
| JP2541693B2 (ja) | 1996-10-09 |
| NO903100D0 (no) | 1990-07-11 |
| DE69026317D1 (de) | 1996-05-09 |
| EP0409614B1 (en) | 1996-04-03 |
| AU630211B2 (en) | 1992-10-22 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MM1K | Lapsed by not paying the annual fees |
Free format text: LAPSED IN JANUARY 2002 |