WO2021124330A8 - System for precision guidance of munitions - Google Patents
System for precision guidance of munitions Download PDFInfo
- Publication number
- WO2021124330A8 WO2021124330A8 PCT/IL2020/051298 IL2020051298W WO2021124330A8 WO 2021124330 A8 WO2021124330 A8 WO 2021124330A8 IL 2020051298 W IL2020051298 W IL 2020051298W WO 2021124330 A8 WO2021124330 A8 WO 2021124330A8
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- projectile
- trajectory
- correction
- camera array
- force generator
- Prior art date
Links
Classifications
-
- 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
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Methods and systems for trajectory correction of a projectile or a munition during flight. The projectile comprises a force generator disposed on a module rotatable around the projectile's longitudinal axis, to generate a force in a direction to correct the trajectory of the projectile. The force generator may have a nozzle, adapted to expel a jet of gas in the desired direction, and a valve for controlling the duration of the expulsion. Guidance of the projectile may be achieved by defining the position of the target on a camera array using a telescopic sight, and detecting an optical signal emitted by an encoded light source, mounted on the projectile, and determining its position in the camera array. Determination of the range of the projectile then enables calculation of the actual trajectory, and if necessary, optically encoded correction signals are sent to the projectile for appropriate trajectory correction.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IL271483A IL271483A (en) | 2019-12-16 | 2019-12-16 | Precision guided low-cost munitions system background |
IL271483 | 2019-12-16 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2021124330A1 WO2021124330A1 (en) | 2021-06-24 |
WO2021124330A8 true WO2021124330A8 (en) | 2022-11-17 |
Family
ID=76477142
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/IL2020/051298 WO2021124330A1 (en) | 2019-12-16 | 2020-12-16 | System for precision guidance of munitions |
Country Status (2)
Country | Link |
---|---|
IL (1) | IL271483A (en) |
WO (1) | WO2021124330A1 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113654412B (en) * | 2021-09-13 | 2024-08-02 | 北京理工大学 | Pulse thrust attitude control device driven by motor |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3317583C2 (en) * | 1983-05-13 | 1986-01-23 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Device with a nozzle arrangement supplied by a propellant source |
GB8618510D0 (en) * | 1986-07-29 | 1986-12-17 | Imi Kynuch Ltd | Guidance apparatus for projectiles |
US5685504A (en) * | 1995-06-07 | 1997-11-11 | Hughes Missile Systems Company | Guided projectile system |
-
2019
- 2019-12-16 IL IL271483A patent/IL271483A/en unknown
-
2020
- 2020-12-16 WO PCT/IL2020/051298 patent/WO2021124330A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
IL271483A (en) | 2021-06-30 |
WO2021124330A1 (en) | 2021-06-24 |
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