SE522565C2 - Förfarande för styrning av en missil - Google Patents
Förfarande för styrning av en missilInfo
- Publication number
- SE522565C2 SE522565C2 SE0004596A SE0004596A SE522565C2 SE 522565 C2 SE522565 C2 SE 522565C2 SE 0004596 A SE0004596 A SE 0004596A SE 0004596 A SE0004596 A SE 0004596A SE 522565 C2 SE522565 C2 SE 522565C2
- Authority
- SE
- Sweden
- Prior art keywords
- missile
- final phase
- trajectory
- phase
- target
- Prior art date
Links
- 238000000034 method Methods 0.000 title claims abstract description 28
- 230000007704 transition Effects 0.000 claims description 24
- 238000009499 grossing Methods 0.000 claims description 4
- 230000008685 targeting Effects 0.000 description 4
- 230000009466 transformation Effects 0.000 description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000014509 gene expression Effects 0.000 description 1
- 150000002500 ions Chemical class 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000010409 ironing Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000001131 transforming 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
- F41G7/22—Homing guidance systems
-
- 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)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (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)
- Catching Or Destruction (AREA)
- Seats For Vehicles (AREA)
- Control Of Vending Devices And Auxiliary Devices For Vending Devices (AREA)
Priority Applications (7)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SE0004596A SE522565C2 (sv) | 2000-12-13 | 2000-12-13 | Förfarande för styrning av en missil |
| ES01270743T ES2233561T3 (es) | 2000-12-13 | 2001-12-11 | Metodo para controlar un misil. |
| PCT/SE2001/002733 WO2002048636A1 (en) | 2000-12-13 | 2001-12-11 | Method for controlling a missile |
| DE60108902T DE60108902T2 (de) | 2000-12-13 | 2001-12-11 | Verfahren zur Lenkung eines Flugkörpers |
| EP01270743A EP1352206B1 (de) | 2000-12-13 | 2001-12-11 | Verfahren zur steuerung eines flugkörpers |
| AT01270743T ATE289052T1 (de) | 2000-12-13 | 2001-12-11 | Verfahren zur steuerung eines flugkörpers |
| AU2002221244A AU2002221244A1 (en) | 2000-12-13 | 2001-12-11 | Method for controlling a missile |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SE0004596A SE522565C2 (sv) | 2000-12-13 | 2000-12-13 | Förfarande för styrning av en missil |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| SE0004596D0 SE0004596D0 (sv) | 2000-12-13 |
| SE0004596L SE0004596L (sv) | 2002-06-14 |
| SE522565C2 true SE522565C2 (sv) | 2004-02-17 |
Family
ID=20282202
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SE0004596A SE522565C2 (sv) | 2000-12-13 | 2000-12-13 | Förfarande för styrning av en missil |
Country Status (7)
| Country | Link |
|---|---|
| EP (1) | EP1352206B1 (de) |
| AT (1) | ATE289052T1 (de) |
| AU (1) | AU2002221244A1 (de) |
| DE (1) | DE60108902T2 (de) |
| ES (1) | ES2233561T3 (de) |
| SE (1) | SE522565C2 (de) |
| WO (1) | WO2002048636A1 (de) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7446291B1 (en) * | 2005-10-03 | 2008-11-04 | Lockheed Martin Corporation | Augmented proportional navigation guidance law using angular acceleration measurements |
| RU2542691C1 (ru) * | 2013-11-22 | 2015-02-20 | Открытое акционерное общество "Конструкторское бюро приборостроения им. академика А.Г. Шипунова" | Способ вывода ракеты в зону захвата цели головкой самонаведения и система для его осуществления (варианты) |
| CN104298246B (zh) * | 2014-09-05 | 2017-02-08 | 湖北航天技术研究院总体设计所 | 一种盘旋飞行轨迹的导引律设计方法及系统 |
| CN108398959A (zh) * | 2018-03-28 | 2018-08-14 | 北京临近空间飞行器系统工程研究所 | 一种高超声速滑翔飞行器快速下压制导控制方法 |
| CN109558685B (zh) * | 2018-12-05 | 2021-07-13 | 北京航空航天大学 | 弹体支点判定方法、装置、存储介质及电子设备 |
| CN111290427B (zh) * | 2018-12-06 | 2021-07-09 | 北京理工大学 | 抗高过载的飞行器侧偏修正系统 |
| US12044506B1 (en) * | 2021-06-15 | 2024-07-23 | Bae Systems Information And Electronic Systems Integration Inc. | Off-axis projectile guidance |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3303763A1 (de) * | 1983-02-04 | 1984-08-09 | Diehl GmbH & Co, 8500 Nürnberg | Verfahren zur zielansteuerung eines projektils und zum bestimmen dessen ballistischer flugbahn sowie vorrichtungen zum ausueben der verfahren |
| FR2626677B1 (fr) * | 1988-02-01 | 1990-06-22 | Thomson Csf | Systeme de radionavigation |
| US5647558A (en) * | 1995-02-14 | 1997-07-15 | Bofors Ab | Method and apparatus for radial thrust trajectory correction of a ballistic projectile |
-
2000
- 2000-12-13 SE SE0004596A patent/SE522565C2/sv not_active IP Right Cessation
-
2001
- 2001-12-11 WO PCT/SE2001/002733 patent/WO2002048636A1/en not_active Ceased
- 2001-12-11 EP EP01270743A patent/EP1352206B1/de not_active Expired - Lifetime
- 2001-12-11 AT AT01270743T patent/ATE289052T1/de not_active IP Right Cessation
- 2001-12-11 DE DE60108902T patent/DE60108902T2/de not_active Expired - Lifetime
- 2001-12-11 ES ES01270743T patent/ES2233561T3/es not_active Expired - Lifetime
- 2001-12-11 AU AU2002221244A patent/AU2002221244A1/en not_active Abandoned
Also Published As
| Publication number | Publication date |
|---|---|
| DE60108902T2 (de) | 2006-03-02 |
| WO2002048636A1 (en) | 2002-06-20 |
| ATE289052T1 (de) | 2005-02-15 |
| SE0004596D0 (sv) | 2000-12-13 |
| EP1352206B1 (de) | 2005-02-09 |
| SE0004596L (sv) | 2002-06-14 |
| AU2002221244A1 (en) | 2002-06-24 |
| DE60108902D1 (de) | 2005-03-17 |
| ES2233561T3 (es) | 2005-06-16 |
| EP1352206A1 (de) | 2003-10-15 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| NUG | Patent has lapsed |