DE69025049D1 - Leichtbau-Flugkörper-Lenksystem - Google Patents
Leichtbau-Flugkörper-LenksystemInfo
- Publication number
- DE69025049D1 DE69025049D1 DE69025049T DE69025049T DE69025049D1 DE 69025049 D1 DE69025049 D1 DE 69025049D1 DE 69025049 T DE69025049 T DE 69025049T DE 69025049 T DE69025049 T DE 69025049T DE 69025049 D1 DE69025049 D1 DE 69025049D1
- Authority
- DE
- Germany
- Prior art keywords
- guidance system
- missile guidance
- lightweight
- lightweight missile
- missile
- 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
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
- G01C21/02—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by astronomical means
- G01C21/025—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by astronomical means with the use of startrackers
-
- 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)
- Physics & Mathematics (AREA)
- Remote Sensing (AREA)
- Radar, Positioning & Navigation (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- General Physics & Mathematics (AREA)
- Astronomy & Astrophysics (AREA)
- Electromagnetism (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Navigation (AREA)
- Details Of Aerials (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/462,181 US5022608A (en) | 1990-01-08 | 1990-01-08 | Lightweight missile guidance system |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69025049D1 true DE69025049D1 (de) | 1996-03-07 |
DE69025049T2 DE69025049T2 (de) | 1996-05-30 |
Family
ID=23835467
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69025049T Expired - Fee Related DE69025049T2 (de) | 1990-01-08 | 1990-12-24 | Leichtbau-Flugkörper-Lenksystem |
Country Status (10)
Country | Link |
---|---|
US (1) | US5022608A (de) |
EP (1) | EP0436215B1 (de) |
JP (1) | JP2638686B2 (de) |
KR (1) | KR940004647B1 (de) |
AU (1) | AU617063B2 (de) |
CA (1) | CA2032267C (de) |
DE (1) | DE69025049T2 (de) |
ES (1) | ES2081904T3 (de) |
IL (1) | IL96671A (de) |
NO (1) | NO300189B1 (de) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5681009A (en) * | 1996-09-27 | 1997-10-28 | Lockheed Missiles And Space Company | Missile having endoatmospheric and exoatmospheric seeker capability |
US6494140B1 (en) | 1999-04-22 | 2002-12-17 | Lockheed Martin Corporation | Modular rocket boosted penetrating warhead |
US6276277B1 (en) | 1999-04-22 | 2001-08-21 | Lockheed Martin Corporation | Rocket-boosted guided hard target penetrator |
US7007888B2 (en) * | 2003-11-25 | 2006-03-07 | The Boeing Company | Inertial position target measuring systems and methods |
IL162863A (en) * | 2004-07-05 | 2012-08-30 | Israel Aerospace Ind Ltd | Exo atmospheric intercepting system and method |
US20060235614A1 (en) * | 2005-04-14 | 2006-10-19 | Starvision Technologies Inc. | Method and Apparatus for Automatic Identification of Celestial Bodies |
US8222582B1 (en) * | 2008-09-30 | 2012-07-17 | Anderson Mark J | Celestial navigation using stellar narrow-band emission |
WO2011002343A1 (en) * | 2009-06-30 | 2011-01-06 | Saab Ab | An extended method for terminal guidance |
US8735788B2 (en) * | 2011-02-18 | 2014-05-27 | Raytheon Company | Propulsion and maneuvering system with axial thrusters and method for axial divert attitude and control |
CN111351401B (zh) * | 2018-12-21 | 2022-12-23 | 北京理工大学 | 应用于捷联导引头制导飞行器的防侧偏制导方法 |
CN110926278B (zh) * | 2019-12-04 | 2021-12-31 | 中国人民解放军海军潜艇学院 | 一种采用多前置角叠加与末端修正的前置导引方法 |
CN111102886B (zh) * | 2019-12-12 | 2022-03-25 | 中国人民解放军海军航空大学 | 一种小微飞行器无陀螺精确制导方法 |
CN111366044B (zh) * | 2019-12-29 | 2022-10-04 | 湖北航天飞行器研究所 | 一种平飞过渡段制导控制方法 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3025023A (en) * | 1954-09-14 | 1962-03-13 | John W B Barghausen | Missile guidance system |
US3499156A (en) * | 1966-02-16 | 1970-03-03 | Goodyear Aerospace Corp | Celestial matching system for attitude stabilization and position determination |
GB1600201A (en) * | 1967-09-11 | 1981-10-14 | British Aerospace | Guidance systems |
SE430102B (sv) * | 1981-10-08 | 1983-10-17 | Saab Scania Ab | Sett och anordning for styrning av en aerodynamisk kropp med skrovfast malsokare |
JPS6052504U (ja) * | 1983-09-12 | 1985-04-13 | 三菱電機株式会社 | 飛しよう体シ−カヘツドセンサ駆動サ−ボ装置 |
JPS6123222A (ja) * | 1984-07-10 | 1986-01-31 | Nec Corp | 誘導方式 |
JPS62125895U (de) * | 1986-01-27 | 1987-08-10 |
-
1990
- 1990-01-08 US US07/462,181 patent/US5022608A/en not_active Expired - Fee Related
- 1990-12-14 IL IL9096671A patent/IL96671A/xx not_active IP Right Cessation
- 1990-12-14 CA CA002032267A patent/CA2032267C/en not_active Expired - Fee Related
- 1990-12-18 AU AU68200/90A patent/AU617063B2/en not_active Ceased
- 1990-12-19 NO NO905476A patent/NO300189B1/no unknown
- 1990-12-24 DE DE69025049T patent/DE69025049T2/de not_active Expired - Fee Related
- 1990-12-24 ES ES90125482T patent/ES2081904T3/es not_active Expired - Lifetime
- 1990-12-24 EP EP90125482A patent/EP0436215B1/de not_active Expired - Lifetime
- 1990-12-27 JP JP2408509A patent/JP2638686B2/ja not_active Expired - Lifetime
- 1990-12-29 KR KR1019900022492A patent/KR940004647B1/ko not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
JP2638686B2 (ja) | 1997-08-06 |
AU6820090A (en) | 1991-07-18 |
JPH04110600A (ja) | 1992-04-13 |
DE69025049T2 (de) | 1996-05-30 |
NO300189B1 (no) | 1997-04-21 |
EP0436215B1 (de) | 1996-01-24 |
IL96671A (en) | 1993-08-18 |
KR910014678A (ko) | 1991-08-31 |
CA2032267A1 (en) | 1991-07-09 |
CA2032267C (en) | 1994-04-19 |
ES2081904T3 (es) | 1996-03-16 |
US5022608A (en) | 1991-06-11 |
EP0436215A3 (en) | 1992-10-28 |
EP0436215A2 (de) | 1991-07-10 |
KR940004647B1 (ko) | 1994-05-27 |
AU617063B2 (en) | 1991-11-14 |
IL96671A0 (en) | 1992-05-25 |
NO905476L (no) | 1991-07-02 |
NO905476D0 (no) | 1990-12-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |