GB989069A - Missile guidance system - Google Patents
Missile guidance systemInfo
- Publication number
- GB989069A GB989069A GB2022554A GB2022554A GB989069A GB 989069 A GB989069 A GB 989069A GB 2022554 A GB2022554 A GB 2022554A GB 2022554 A GB2022554 A GB 2022554A GB 989069 A GB989069 A GB 989069A
- Authority
- GB
- United Kingdom
- Prior art keywords
- missiles
- aircraft
- target
- missile
- guidance system
- 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)
- Radar Systems Or Details Thereof (AREA)
Abstract
989,069. Self propelled missiles. SPERRY RAND CORPORATION. July 9, 1954, No. 20225/54. Drawings to Specification. Heading F3A. [Also in Divisions G3 and H4] An aircraft which carries beam riding, air-toair missiles is controlled by the pilot so as to launch missiles at a moving target. The target is detected by the aircraft through a pulse radar having a conically swept beam. The missile rides within the beam, which has four quadrants distinguished from each other by a pulse sequence transmitted with the radar signals. The missiles have an ogive nose and cruciform wings and tail surfaces. They are provided with a proximity fuse, a warhead, a microwave receiver, a control servo system and a solid fuel motor. Specifications 621,836, 635,478, 767,831, 812,533, 834,520 and 989,070 are referred to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2022554A GB989069A (en) | 1954-07-09 | 1954-07-09 | Missile guidance system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2022554A GB989069A (en) | 1954-07-09 | 1954-07-09 | Missile guidance system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB989069A true GB989069A (en) | 1965-04-14 |
Family
ID=10142455
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2022554A Expired GB989069A (en) | 1954-07-09 | 1954-07-09 | Missile guidance system |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB989069A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115345377A (en) * | 2022-08-29 | 2022-11-15 | 中国兵器科学研究院 | Position prediction method and device, electronic equipment and storage medium |
| CN116499444A (en) * | 2023-06-20 | 2023-07-28 | 中国船舶集团有限公司第七〇七研究所 | Hemispherical resonant gyro mode switching method based on vibration mode active precession |
-
1954
- 1954-07-09 GB GB2022554A patent/GB989069A/en not_active Expired
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115345377A (en) * | 2022-08-29 | 2022-11-15 | 中国兵器科学研究院 | Position prediction method and device, electronic equipment and storage medium |
| CN115345377B (en) * | 2022-08-29 | 2023-09-01 | 中国兵器科学研究院 | Position prediction method and device, electronic equipment and storage medium |
| CN116499444A (en) * | 2023-06-20 | 2023-07-28 | 中国船舶集团有限公司第七〇七研究所 | Hemispherical resonant gyro mode switching method based on vibration mode active precession |
| CN116499444B (en) * | 2023-06-20 | 2023-09-05 | 中国船舶集团有限公司第七〇七研究所 | Hemispherical resonant gyro mode switching method based on vibration mode active precession |
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