GB610803A - Improvements in or relating to radio-controlled projectiles - Google Patents
Improvements in or relating to radio-controlled projectilesInfo
- Publication number
- GB610803A GB610803A GB6529/42A GB652942A GB610803A GB 610803 A GB610803 A GB 610803A GB 6529/42 A GB6529/42 A GB 6529/42A GB 652942 A GB652942 A GB 652942A GB 610803 A GB610803 A GB 610803A
- Authority
- GB
- United Kingdom
- Prior art keywords
- projectile
- radiator
- controlled
- gun
- target
- 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
Links
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
- F41G7/24—Beam riding guidance systems
Landscapes
- Engineering & Computer Science (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)
Abstract
610,803. Automatic control systems for guiding projectiles. SPERRY GYROSCOPE CO., Inc. May 13, 1942, No. 6529. Convention date, July 8, 1941. [Class 38 (iv)] [Also in Group XL (c)] The directional radiator for guiding a projectile towards its target is controlled by a predictor system. As shown, the predictor 172 by means of selsyn transmission systems of known kind controls a gun 185 in altitude and azimuth and at the same time the radiator 171. Manual means 186, 187 allow the radiator to be moved independently of the gun when the projectile is near its target. The projectile is provided with aerials at spaced points and these in accordance with the energy that they receive, control valves causing blasts of compressed air or carbon dioxide to be emitted in the direction to keep the projectile to the beam. Alternatively, the projectile may be controlled by adjustable fins.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US610803XA | 1941-07-08 | 1941-07-08 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB610803A true GB610803A (en) | 1948-10-21 |
Family
ID=22033475
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB6529/42A Expired GB610803A (en) | 1941-07-08 | 1942-05-13 | Improvements in or relating to radio-controlled projectiles |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB610803A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112731458A (en) * | 2020-12-24 | 2021-04-30 | 彩虹无人机科技有限公司 | Method for measuring missile launching direction |
-
1942
- 1942-05-13 GB GB6529/42A patent/GB610803A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112731458A (en) * | 2020-12-24 | 2021-04-30 | 彩虹无人机科技有限公司 | Method for measuring missile launching direction |
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