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
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
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US3883091A (en) | Guided missile control systems | |
| GB1116801A (en) | Improvements in or relating to homing systems | |
| GB1218472A (en) | Automatic pilot systems for aircraft | |
| GB1062473A (en) | Process for controlling the motion of a first body as a function of the position of a second body, and device for implementing this process | |
| GB1486537A (en) | Guided missile system | |
| GB1432933A (en) | Guidance and control system for target-seeking devices | |
| EP0222571A3 (en) | Line of sight missile guidance | |
| GB1441127A (en) | Guidance system for an anti-aircraft missile | |
| GB1301041A (en) | Improvements relating to vehicle command systems | |
| GB1014970A (en) | Improvements in and relating to the guiding of a remote controlled missile towards afreely movable target | |
| GB1203412A (en) | Improvements relating to missile guidance systems | |
| GB1056815A (en) | Fire control system for weapons | |
| GB1377358A (en) | Method of advancing the point of impact for passive-location missiles guided by means of proportional navigation in the self-guide phase | |
| GB945613A (en) | Improvements in guidance systems for missiles and other moving bodies | |
| GB1064774A (en) | Weapon firing control system | |
| GB1062530A (en) | Aircraft control arrangements | |
| GB1272402A (en) | Radar installation | |
| GB1149435A (en) | Method of homing and guiding flying bodies | |
| GB1148354A (en) | Improvements in or relating to control apparatus for use in aircraft | |
| GB942133A (en) | Improvements in or relating to radar tracking systems | |
| GB1434305A (en) | Aircraft control system using inertial signals | |
| GB943310A (en) | Improvements in or relating to automatic control systems for guiding air-borne missiles | |
| GB1605342A (en) | Improvements relating to missile guidance systems | |
| GB1446362A (en) | Navigation system for guiding a body to impact a moving target | |
| GB1204481A (en) | Improvements relating to take-off director systems for aircraft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed | ||
| PLNP | Patent lapsed through nonpayment of renewal fees |