DE3802551A1 - Verfahren zum korrigieren der flugbahn eines flugkoerpers sowie flugkoerper zur durchfuehrung dieses verfahrens - Google Patents
Verfahren zum korrigieren der flugbahn eines flugkoerpers sowie flugkoerper zur durchfuehrung dieses verfahrensInfo
- Publication number
- DE3802551A1 DE3802551A1 DE3802551A DE3802551A DE3802551A1 DE 3802551 A1 DE3802551 A1 DE 3802551A1 DE 3802551 A DE3802551 A DE 3802551A DE 3802551 A DE3802551 A DE 3802551A DE 3802551 A1 DE3802551 A1 DE 3802551A1
- Authority
- DE
- Germany
- Prior art keywords
- missile
- correction
- flight
- force
- trajectory
- 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
- 238000000034 method Methods 0.000 title claims abstract description 34
- 238000012937 correction Methods 0.000 claims abstract description 69
- 230000008569 process Effects 0.000 claims abstract description 13
- 230000005484 gravity Effects 0.000 claims description 8
- 238000005096 rolling process Methods 0.000 claims description 6
- 230000009471 action Effects 0.000 claims description 2
- 238000006243 chemical reaction Methods 0.000 claims description 2
- 230000010355 oscillation Effects 0.000 abstract description 15
- 238000005452 bending Methods 0.000 abstract 1
- 230000005284 excitation Effects 0.000 description 5
- 230000008901 benefit Effects 0.000 description 3
- 238000013016 damping Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000005259 measurement Methods 0.000 description 3
- 230000004044 response Effects 0.000 description 3
- 238000003860 storage Methods 0.000 description 3
- 241000272525 Anas platyrhynchos Species 0.000 description 2
- 101100400378 Mus musculus Marveld2 gene Proteins 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 238000000418 atomic force spectrum Methods 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000009795 derivation Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 238000005286 illumination Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 230000009191 jumping Effects 0.000 description 1
- 210000003734 kidney Anatomy 0.000 description 1
- 210000004072 lung Anatomy 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000006386 neutralization reaction Methods 0.000 description 1
- 230000003472 neutralizing effect Effects 0.000 description 1
- 230000003534 oscillatory effect Effects 0.000 description 1
- 230000001629 suppression Effects 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 230000001960 triggered effect Effects 0.000 description 1
- 238000009966 trimming Methods 0.000 description 1
Classifications
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/60—Steering arrangements
- F42B10/66—Steering by varying intensity or direction of thrust
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Fluid Mechanics (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE3802551A DE3802551A1 (de) | 1988-01-28 | 1988-01-28 | Verfahren zum korrigieren der flugbahn eines flugkoerpers sowie flugkoerper zur durchfuehrung dieses verfahrens |
| FR8900897A FR2626664B1 (fr) | 1988-01-28 | 1989-01-25 | Procede de correction de la trajectoire d'un engin et engins concus pour l'application de ce procede |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE3802551A DE3802551A1 (de) | 1988-01-28 | 1988-01-28 | Verfahren zum korrigieren der flugbahn eines flugkoerpers sowie flugkoerper zur durchfuehrung dieses verfahrens |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| DE3802551A1 true DE3802551A1 (de) | 1989-08-10 |
| DE3802551C2 DE3802551C2 (enrdf_load_stackoverflow) | 1991-01-17 |
Family
ID=6346186
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE3802551A Granted DE3802551A1 (de) | 1988-01-28 | 1988-01-28 | Verfahren zum korrigieren der flugbahn eines flugkoerpers sowie flugkoerper zur durchfuehrung dieses verfahrens |
Country Status (2)
| Country | Link |
|---|---|
| DE (1) | DE3802551A1 (enrdf_load_stackoverflow) |
| FR (1) | FR2626664B1 (enrdf_load_stackoverflow) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5836540A (en) * | 1994-03-25 | 1998-11-17 | Rheinmetall W & M Gmbh | Projectile having an apparatus for flight-path correction |
| NO20160105A1 (en) * | 2016-01-20 | 2017-07-21 | FLIR Unmanned Aerial Systems AS | Resonant Operating Rotor Assembly |
| CN111026139A (zh) * | 2019-09-25 | 2020-04-17 | 中国人民解放军63850部队 | 一种基于飞行轨迹的三维模型姿态调整控制方法 |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2364164A1 (fr) * | 1976-09-08 | 1978-04-07 | Stauff Emile | Dispositif de pilotage d'un projectile en auto-rotation |
| DE3024842A1 (de) * | 1980-07-01 | 1982-01-28 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Einrichtung zur lenkung eines um seine laengsachse rotierenden flugkoerpers |
| DE2714688C2 (de) * | 1976-04-02 | 1986-06-12 | Aktiebolaget Bofors, Bofors | Vorrichtung zur Korrektur der Flugbahn eines Projektils |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2504703B1 (fr) * | 1981-04-24 | 1986-09-05 | Stauff Emile | Systeme d'asservissement d'un projectile a une reference axiale pour supprimer l'effet du vent |
| US4659035A (en) * | 1985-01-25 | 1987-04-21 | The United States As Represented By The Secretary Of The Navy | Rate estimation by mixing two independent rate signals |
-
1988
- 1988-01-28 DE DE3802551A patent/DE3802551A1/de active Granted
-
1989
- 1989-01-25 FR FR8900897A patent/FR2626664B1/fr not_active Expired - Fee Related
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2714688C2 (de) * | 1976-04-02 | 1986-06-12 | Aktiebolaget Bofors, Bofors | Vorrichtung zur Korrektur der Flugbahn eines Projektils |
| FR2364164A1 (fr) * | 1976-09-08 | 1978-04-07 | Stauff Emile | Dispositif de pilotage d'un projectile en auto-rotation |
| DE3024842A1 (de) * | 1980-07-01 | 1982-01-28 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Einrichtung zur lenkung eines um seine laengsachse rotierenden flugkoerpers |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5836540A (en) * | 1994-03-25 | 1998-11-17 | Rheinmetall W & M Gmbh | Projectile having an apparatus for flight-path correction |
| NO20160105A1 (en) * | 2016-01-20 | 2017-07-21 | FLIR Unmanned Aerial Systems AS | Resonant Operating Rotor Assembly |
| NO341222B1 (en) * | 2016-01-20 | 2017-09-18 | FLIR Unmanned Aerial Systems AS | Resonant Operating Rotor Assembly |
| US10960974B2 (en) | 2016-01-20 | 2021-03-30 | FLIR Unmanned Aerial Systems AS | Resonant operating rotor assembly |
| CN111026139A (zh) * | 2019-09-25 | 2020-04-17 | 中国人民解放军63850部队 | 一种基于飞行轨迹的三维模型姿态调整控制方法 |
| CN111026139B (zh) * | 2019-09-25 | 2023-07-18 | 中国人民解放军63850部队 | 一种基于飞行轨迹的三维模型姿态调整控制方法 |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2626664A1 (fr) | 1989-08-04 |
| DE3802551C2 (enrdf_load_stackoverflow) | 1991-01-17 |
| FR2626664B1 (fr) | 1993-07-30 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| OP8 | Request for examination as to paragraph 44 patent law | ||
| D2 | Grant after examination | ||
| 8364 | No opposition during term of opposition | ||
| 8339 | Ceased/non-payment of the annual fee |