EP0331804A3 - Projectile à guidage en phase terminale - Google Patents
Projectile à guidage en phase terminale Download PDFInfo
- Publication number
- EP0331804A3 EP0331804A3 EP19880120227 EP88120227A EP0331804A3 EP 0331804 A3 EP0331804 A3 EP 0331804A3 EP 19880120227 EP19880120227 EP 19880120227 EP 88120227 A EP88120227 A EP 88120227A EP 0331804 A3 EP0331804 A3 EP 0331804A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- projectile
- detector
- air bearing
- wedge
- optical
- 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.)
- Granted
Links
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
- F41G7/22—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
-
- 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
- F41G7/2213—Homing guidance systems maintaining the axis of an orientable seeking head pointed at the target, e.g. target seeking gyro
-
- 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
- F41G7/222—Homing guidance systems for spin-stabilized 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
- F41G7/22—Homing guidance systems
- F41G7/2253—Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Telescopes (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3807725A DE3807725A1 (de) | 1988-03-09 | 1988-03-09 | Endphasengelenktes geschoss |
DE3807725 | 1988-03-09 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0331804A2 EP0331804A2 (fr) | 1989-09-13 |
EP0331804A3 true EP0331804A3 (fr) | 1991-07-31 |
EP0331804B1 EP0331804B1 (fr) | 1994-10-19 |
Family
ID=6349248
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP88120227A Expired - Lifetime EP0331804B1 (fr) | 1988-03-09 | 1988-12-03 | Projectile à guidage en phase terminale |
Country Status (3)
Country | Link |
---|---|
US (1) | US4917330A (fr) |
EP (1) | EP0331804B1 (fr) |
DE (2) | DE3807725A1 (fr) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4033948A1 (de) * | 1990-10-25 | 1992-04-30 | Bodenseewerk Geraetetech | Sucher zur abtastung eines gesichtsfeldes |
DE4226024C1 (fr) * | 1992-08-06 | 1993-07-15 | Bodenseewerk Geraetetechnik Gmbh, 7770 Ueberlingen, De | |
DE4325589B4 (de) * | 1993-07-30 | 2007-11-22 | Diehl Bgt Defence Gmbh & Co. Kg | Zielsuchkopf für Lenkflugkörper oder Geschosse |
DE19611595B4 (de) * | 1996-03-23 | 2004-02-05 | BODENSEEWERK GERäTETECHNIK GMBH | Suchkopf für zielverfolgende Flugkörper oder Geschosse |
DE19953701C2 (de) * | 1999-11-08 | 2002-01-24 | Lfk Gmbh | Verfahren und Vorrichtungen zur Verminderung von Druck und Temperatur auf der Vorderseite eines Flugkörpers bei Überschallgeschwindigkeit |
IL143694A (en) | 2001-06-12 | 2006-10-31 | Geo T Vision Ltd | Projectile fuse imaging device and method |
US7943914B2 (en) * | 2003-05-30 | 2011-05-17 | Bae Systems Information And Electronic Systems Integration, Inc. | Back illumination method for counter measuring IR guided missiles |
US7718936B2 (en) * | 2004-06-03 | 2010-05-18 | Lockheed Martin Corporation | Bulk material windows for distributed aperture sensors |
US20060054660A1 (en) * | 2004-09-10 | 2006-03-16 | Honeywell International Inc. | Articulated gas bearing support pads |
US7274439B2 (en) * | 2004-09-10 | 2007-09-25 | Honeywell International Inc. | Precise, no-contact, position sensing using imaging |
US7698064B2 (en) * | 2004-09-10 | 2010-04-13 | Honeywell International Inc. | Gas supported inertial sensor system and method |
US7295947B2 (en) * | 2004-09-10 | 2007-11-13 | Honeywell International Inc. | Absolute position determination of an object using pattern recognition |
US7617070B2 (en) * | 2004-09-10 | 2009-11-10 | Honeywell International Inc. | Absolute position determination of an object using pattern recognition |
US7340344B2 (en) * | 2004-09-10 | 2008-03-04 | Honeywell International Inc. | Spherical position monitoring system |
US7289902B2 (en) * | 2004-09-10 | 2007-10-30 | Honeywell International Inc. | Three dimensional balance assembly |
US7458264B2 (en) * | 2004-09-10 | 2008-12-02 | Honeywell International Inc. | Generalized inertial measurement error reduction through multiple axis rotation during flight |
US7366613B2 (en) * | 2004-09-10 | 2008-04-29 | Honeywell International Inc. | RF wireless communication for deeply embedded aerospace systems |
US7647176B2 (en) * | 2007-01-11 | 2010-01-12 | Honeywell International Inc. | Method and system for wireless power transfers through multiple ports |
US7425097B1 (en) | 2007-07-17 | 2008-09-16 | Honeywell International Inc. | Inertial measurement unit with wireless power transfer gap control |
US7762133B2 (en) * | 2007-07-17 | 2010-07-27 | Honeywell International Inc. | Inertial measurement unit with gas plenums |
US7671607B2 (en) * | 2007-09-06 | 2010-03-02 | Honeywell International Inc. | System and method for measuring air bearing gap distance |
US8686326B1 (en) * | 2008-03-26 | 2014-04-01 | Arete Associates | Optical-flow techniques for improved terminal homing and control |
DE102009029895B4 (de) * | 2009-06-23 | 2018-01-25 | Diehl Defence Gmbh & Co. Kg | Optisches System für einen Flugkörper und Verfahren zum Abbilden eines Gegenstands |
US8921748B2 (en) * | 2011-05-19 | 2014-12-30 | Lockheed Martin Corporation | Optical window and detection system employing the same |
US9568280B1 (en) | 2013-11-25 | 2017-02-14 | Lockheed Martin Corporation | Solid nose cone and related components |
DE102014002822A1 (de) * | 2014-02-26 | 2015-08-27 | Diehl Bgt Defence Gmbh & Co. Kg | Verfahren zum Start eines Lenkflugkörpers und Flugkörpersystem |
US9534868B1 (en) | 2014-06-03 | 2017-01-03 | Lockheed Martin Corporation | Aerodynamic conformal nose cone and scanning mechanism |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4155521A (en) * | 1975-12-08 | 1979-05-22 | The Singer Company | Cannon launched platform |
US4500051A (en) * | 1972-10-06 | 1985-02-19 | Texas Instruments Incorporated | Gyro stabilized optics with fixed detector |
DE3438544A1 (de) * | 1984-10-20 | 1986-04-24 | Bodenseewerk Geraetetech | Optischer sucher |
EP0233080A2 (fr) * | 1986-02-11 | 1987-08-19 | Raytheon Company | Autodirecteur infrarouge |
DE3644456C1 (de) * | 1986-12-24 | 1988-01-21 | Rheinmetall Gmbh | Geschoss |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2816721A (en) * | 1953-09-15 | 1957-12-17 | Taylor Richard John | Rocket powered aerial vehicle |
US2990699A (en) * | 1958-12-08 | 1961-07-04 | Specialties Dev Corp | Cooling apparatus |
US4009393A (en) * | 1967-09-14 | 1977-02-22 | General Dynamics Corporation | Dual spectral range target tracking seeker |
US3920200A (en) * | 1973-12-06 | 1975-11-18 | Singer Co | Projectile having a gyroscope |
US4004754A (en) * | 1974-07-11 | 1977-01-25 | The United States Of America As Represented By The Secretary Of The Army | High-speed, high-G air bearing optical mount for Rosette scan generator |
US4034807A (en) * | 1975-08-12 | 1977-07-12 | Edgar N. Prince | Inside pipe wiper |
US4009848A (en) * | 1975-10-15 | 1977-03-01 | The Singer Company | Gyro seeker |
US4039246A (en) * | 1976-01-22 | 1977-08-02 | General Dynamics Corporation | Optical scanning apparatus with two mirrors rotatable about a common axis |
DE2921228C3 (de) * | 1979-05-25 | 1981-11-26 | Bodenseewerk Gerätetechnik GmbH, 7770 Überlingen | Zielsuchkopf für einen Flugkörper |
DE2923547C2 (de) * | 1979-06-09 | 1981-04-09 | Bodenseewerk Gerätetechnik GmbH, 7770 Überlingen | Zielsuchvorrichtung für Flugkörper |
US4413177A (en) * | 1981-11-30 | 1983-11-01 | Ford Motor Company | Optical scanning apparatus incorporating counter-rotation of primary and secondary scanning elements about a common axis by a common driving source |
DE3505198C1 (de) * | 1985-02-15 | 1986-07-24 | Bodenseewerk Gerätetechnik GmbH, 7770 Überlingen | Vorrichtung zur Abtastung eines Gesichtsfeldes |
DE3642683A1 (de) * | 1986-12-13 | 1988-06-16 | Bodenseewerk Geraetetech | Kryostat zur kuehlung eines detektors |
-
1988
- 1988-03-09 DE DE3807725A patent/DE3807725A1/de not_active Withdrawn
- 1988-12-03 EP EP88120227A patent/EP0331804B1/fr not_active Expired - Lifetime
- 1988-12-03 DE DE3851880T patent/DE3851880D1/de not_active Expired - Fee Related
-
1989
- 1989-03-03 US US07/319,323 patent/US4917330A/en not_active Expired - Fee Related
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4500051A (en) * | 1972-10-06 | 1985-02-19 | Texas Instruments Incorporated | Gyro stabilized optics with fixed detector |
US4155521A (en) * | 1975-12-08 | 1979-05-22 | The Singer Company | Cannon launched platform |
DE3438544A1 (de) * | 1984-10-20 | 1986-04-24 | Bodenseewerk Geraetetech | Optischer sucher |
EP0233080A2 (fr) * | 1986-02-11 | 1987-08-19 | Raytheon Company | Autodirecteur infrarouge |
DE3644456C1 (de) * | 1986-12-24 | 1988-01-21 | Rheinmetall Gmbh | Geschoss |
Also Published As
Publication number | Publication date |
---|---|
DE3851880D1 (de) | 1994-11-24 |
US4917330A (en) | 1990-04-17 |
EP0331804B1 (fr) | 1994-10-19 |
EP0331804A2 (fr) | 1989-09-13 |
DE3807725A1 (de) | 1989-09-21 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0331804A3 (fr) | Projectile à guidage en phase terminale | |
US4611771A (en) | Fiber optic track/reaim system | |
DE2533697A1 (de) | Einrichtung zur signaluebertragung zwischen einer abschussbasis und einem flugkoerper mittels einer lichtuebertragungsstrecke | |
DE2336040B2 (de) | Abwehrsystem, mit mehreren Geschossen | |
AU2462888A (en) | Optical gun sight | |
CH693863A5 (de) | Anordnung zur Flugbahnkorrektur von Flugkorpern. | |
JPS5430854A (en) | Two-dimensional scanner | |
SE9403070L (sv) | Sökare för målförföljande missiler | |
US4103847A (en) | Line scan area signature detection method | |
DE1623438C3 (fr) | ||
DE1623438B2 (de) | übungsgerät für das Lenken von Fernlenkgeschossen | |
CH468615A (de) | Lichtsignal-Rundum-Empfänger | |
US4967979A (en) | Command guidance technique for line-of-sight missile | |
EP1120624A3 (fr) | Dispositif de poursuite de missile | |
US3494576A (en) | Self-contained and automatic guidance system for directing a missile towards a radiation-emitting target | |
GB1222694A (en) | An aiming and follow-up device for remote controlled jet-propelled missiles | |
US3518368A (en) | Apparatus and information processing methods for a tracking system tracker unit | |
US3706429A (en) | Missile proportional navigation system using fixed seeker | |
FR2412812A1 (fr) | Dispositif permettant de modifier la trajectoire d'un projectile | |
EP0795759B1 (fr) | Missile pour détecter et attaquer des hélicopters hostiles | |
DE68911191T2 (de) | Stabilisierungsvorrichtung für Geschosse von gezogenen Läufen. | |
DE4423758A1 (de) | Vorrichtung zum Erfassen von Hubschraubern | |
DE4325589B4 (de) | Zielsuchkopf für Lenkflugkörper oder Geschosse | |
DE1798069C1 (de) | Verfahren und Anordnung zur Unterdrueckung von Stoerzielen | |
Hessman | Airslew Anti-Armor Weapon Concept |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): DE FR GB IT |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
AK | Designated contracting states |
Kind code of ref document: A3 Designated state(s): DE FR GB IT |
|
17P | Request for examination filed |
Effective date: 19920127 |
|
17Q | First examination report despatched |
Effective date: 19920807 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): DE FR GB IT |
|
REF | Corresponds to: |
Ref document number: 3851880 Country of ref document: DE Date of ref document: 19941124 |
|
ITF | It: translation for a ep patent filed |
Owner name: STUDIO JAUMANN |
|
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 19950113 |
|
ET | Fr: translation filed | ||
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed | ||
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 19981110 Year of fee payment: 11 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 19981119 Year of fee payment: 11 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 19990227 Year of fee payment: 11 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 19991203 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 19991203 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20000831 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20001003 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED. Effective date: 20051203 |