GB1203412A - Improvements relating to missile guidance systems - Google Patents
Improvements relating to missile guidance systemsInfo
- Publication number
- GB1203412A GB1203412A GB903166A GB903166A GB1203412A GB 1203412 A GB1203412 A GB 1203412A GB 903166 A GB903166 A GB 903166A GB 903166 A GB903166 A GB 903166A GB 1203412 A GB1203412 A GB 1203412A
- Authority
- GB
- United Kingdom
- Prior art keywords
- missile
- roll
- ground
- tracker
- 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
- F41G7/30—Command link guidance systems
- F41G7/301—Details
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)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
1,203,412. Automatic steering control. BRITISH AIRCRAFT CORP. Ltd. June 1, 1967 [March 1, 1966], No.9031/66. Heading G3R. In a missile control system, in which the missile is guided towards a target by a ground tracking device, the control signals transmitted to the missile are adjusted, at the tracking device, for the missile roll charges. The ground tracker provides missile control signals corresponding to the angular separation between the target and missile in azimuth and elevation The control signals are passed through a missile roll resolver located at the ground tracker before transmission to the missile. The roll resolver is continuously adjusted by signals from models of the missile pitch and your guidance loops, sited at the ground tracker. The angle of resolution of the resolver is approximately equal to the missile roll angle at all times, the model loops being supplied from the tracker with target tracking signals.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB903166A GB1203412A (en) | 1966-03-01 | 1966-03-01 | Improvements relating to missile guidance systems |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB903166A GB1203412A (en) | 1966-03-01 | 1966-03-01 | Improvements relating to missile guidance systems |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1203412A true GB1203412A (en) | 1970-08-26 |
Family
ID=9864059
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB903166A Expired GB1203412A (en) | 1966-03-01 | 1966-03-01 | Improvements relating to missile guidance systems |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB1203412A (en) |
-
1966
- 1966-03-01 GB GB903166A patent/GB1203412A/en not_active Expired
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed | ||
| PLNP | Patent lapsed through nonpayment of renewal fees |