FR2642515B1 - Procede de defense antiaerienne - Google Patents
Procede de defense antiaerienneInfo
- Publication number
- FR2642515B1 FR2642515B1 FR8703325A FR8703325A FR2642515B1 FR 2642515 B1 FR2642515 B1 FR 2642515B1 FR 8703325 A FR8703325 A FR 8703325A FR 8703325 A FR8703325 A FR 8703325A FR 2642515 B1 FR2642515 B1 FR 2642515B1
- Authority
- FR
- France
- Prior art keywords
- air defense
- defense process
- air
- defense
- 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 - Fee Related
Links
- 230000007123 defense Effects 0.000 title 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/34—Direction control systems for self-propelled missiles based on predetermined target position data
- F41G7/343—Direction control systems for self-propelled missiles based on predetermined target position data comparing observed and stored data of target position or of distinctive marks along the path towards the target
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/008—Combinations of different guidance systems
-
- 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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Remote Sensing (AREA)
- Radar, Positioning & Navigation (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Electromagnetism (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 |
---|---|---|---|
DE3608108A DE3608108C1 (de) | 1986-03-12 | 1986-03-12 | Verfahren zur Abwehr von Flugobjekten |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2642515A1 FR2642515A1 (fr) | 1990-08-03 |
FR2642515B1 true FR2642515B1 (fr) | 1993-03-26 |
Family
ID=6296086
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8703325A Expired - Fee Related FR2642515B1 (fr) | 1986-03-12 | 1987-03-11 | Procede de defense antiaerienne |
Country Status (4)
Country | Link |
---|---|
US (1) | US5050818A (fr) |
DE (1) | DE3608108C1 (fr) |
FR (1) | FR2642515B1 (fr) |
GB (1) | GB2229294B (fr) |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4123308C2 (de) * | 1991-07-13 | 1993-12-23 | Diehl Gmbh & Co | Lenkbares Projektil gegen Luftziele |
DE4201572C2 (de) * | 1992-01-22 | 1994-07-14 | Deutsche Aerospace | Zieldeckungs-Lenkung mit adaptierbarem Flugkörper-Geschwindigkeits-Profil |
FR2712972B1 (fr) * | 1993-11-25 | 1996-01-26 | Aerospatiale | Système de défense antiaérien et missile de défense pour un tel système. |
EP0687885B1 (fr) * | 1993-12-01 | 1998-09-16 | Konstruktorskoe Bjuro Mashinostroenia | Systeme d'autodefense pour vehicule |
DE4426014B4 (de) * | 1994-07-22 | 2004-09-30 | Diehl Stiftung & Co.Kg | System zum Schutz eines Zieles gegen Flugkörper |
US5710423A (en) * | 1996-09-27 | 1998-01-20 | Mcdonnell Douglas Corporation | Exo-atmospheric missile intercept system employing tandem interceptors to overcome unfavorable sun positions |
DE19724773C2 (de) * | 1997-06-12 | 1999-05-12 | Diehl Stiftung & Co | Wecksensor, insbesondere für eine Zielverfolgungseinrichtung |
SE510183C2 (sv) * | 1998-01-28 | 1999-04-26 | Saab Dynamics Ab | Metod och anordning för styrning av en robot mot ett rörligt mål |
US20030045884A1 (en) * | 2001-09-04 | 2003-03-06 | Bruce Robie | Instrument and system for preparing the disc space between two vertebral bodies |
US7066427B2 (en) * | 2004-02-26 | 2006-06-27 | Chang Industry, Inc. | Active protection device and associated apparatus, system, and method |
US7104496B2 (en) * | 2004-02-26 | 2006-09-12 | Chang Industry, Inc. | Active protection device and associated apparatus, system, and method |
DE102004037235A1 (de) * | 2004-07-31 | 2006-03-23 | Diehl Bgt Defence Gmbh & Co. Kg | Verfahren zum Schützen einer Immobilie gegen ein angreifendes Projektil |
IL163609A (en) * | 2004-08-19 | 2011-12-29 | Israel Aerospace Ind Ltd | Method for obtaining a sky view of a battle site |
US7387060B1 (en) * | 2005-05-17 | 2008-06-17 | The United States Of America As Represented By The Secretary Of The Navy | Rocket exhaust defense system and method |
US8130137B1 (en) | 2005-07-26 | 2012-03-06 | Lockheed Martin Corporation | Template updated boost algorithm |
US7566026B2 (en) * | 2006-03-29 | 2009-07-28 | Raytheon Company | Onboard guidance method for ballistic missiles |
US7473876B1 (en) * | 2006-05-09 | 2009-01-06 | Lockheed Martin Corporation | Boost phase intercept missile fire control system architecture |
US7977614B2 (en) * | 2006-09-03 | 2011-07-12 | E.C.S. Engineering Consulting Services-Aerospace Ltd. | Method and system for defense against incoming rockets and missiles |
US8134103B2 (en) * | 2006-12-27 | 2012-03-13 | Lockheed Martin Corporation | Burnout time estimation and early thrust termination determination for a boosting target |
US8288696B1 (en) * | 2007-07-26 | 2012-10-16 | Lockheed Martin Corporation | Inertial boost thrust vector control interceptor guidance |
US8380367B2 (en) * | 2009-03-26 | 2013-02-19 | The University Of North Dakota | Adaptive surveillance and guidance system for vehicle collision avoidance and interception |
FR2945624B1 (fr) * | 2009-05-15 | 2011-06-10 | Mbda France | Procede et systeme d'estimation d'une trajectoire d'un mobile |
CN102087082B (zh) * | 2010-11-22 | 2013-05-08 | 北京机械设备研究所 | 一种基于射表拟合的低空慢速小目标拦截方法 |
US12044506B1 (en) * | 2021-06-15 | 2024-07-23 | Bae Systems Information And Electronic Systems Integration Inc. | Off-axis projectile guidance |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1108083B (de) * | 1954-02-23 | 1961-05-31 | Ericsson Telefon Ab L M | Vorrichtung zum Vorherbestimmen der wahrscheinlichen Bewegungsbahnen von Flugkoerpern |
US4171818A (en) * | 1977-04-04 | 1979-10-23 | Ferrofluidics Corporation | Dynamic lip seal using ferrofluids as sealant/lubricant |
US4277038A (en) * | 1979-04-27 | 1981-07-07 | The United States Of America As Represented By The Secretary Of The Army | Trajectory shaping of anti-armor missiles via tri-mode guidance |
CA1242516A (fr) * | 1982-04-21 | 1988-09-27 | William H. Bell | Systeme d'orme a guidage jusqu'au point d'impact |
US4641801A (en) * | 1982-04-21 | 1987-02-10 | Lynch Jr David D | Terminally guided weapon delivery system |
DE3238293A1 (de) * | 1982-10-15 | 1984-04-19 | Siemens AG, 1000 Berlin und 8000 München | Schaltungsanordnung zur verarbeitung von zieldaten |
US4609988A (en) * | 1983-03-17 | 1986-09-02 | Sperry Corporation | Automatic prediction and capture of a preselected altitude for aircraft |
GB2140538A (en) * | 1983-05-17 | 1984-11-28 | Ferranti Plc | Projectile guidance system |
DE3435634A1 (de) * | 1984-09-28 | 1986-04-10 | Diehl GmbH & Co, 8500 Nürnberg | Zielerfassungseinrichtung fuer flugkoerper |
-
1986
- 1986-03-12 DE DE3608108A patent/DE3608108C1/de not_active Expired - Lifetime
-
1987
- 1987-01-13 GB GB8700679A patent/GB2229294B/en not_active Expired - Fee Related
- 1987-03-11 FR FR8703325A patent/FR2642515B1/fr not_active Expired - Fee Related
-
1989
- 1989-03-02 US US07/321,663 patent/US5050818A/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
GB2229294B (en) | 1990-11-28 |
GB2229294A (en) | 1990-09-19 |
US5050818A (en) | 1991-09-24 |
FR2642515A1 (fr) | 1990-08-03 |
DE3608108C1 (de) | 1990-06-07 |
GB8700679D0 (en) | 1990-05-16 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |