SE8605338D0 - DEVICE FOR GENERATING DELAY IN SLIDABLE DEVICE - Google Patents
DEVICE FOR GENERATING DELAY IN SLIDABLE DEVICEInfo
- Publication number
- SE8605338D0 SE8605338D0 SE8605338A SE8605338A SE8605338D0 SE 8605338 D0 SE8605338 D0 SE 8605338D0 SE 8605338 A SE8605338 A SE 8605338A SE 8605338 A SE8605338 A SE 8605338A SE 8605338 D0 SE8605338 D0 SE 8605338D0
- Authority
- SE
- Sweden
- Prior art keywords
- target
- missile
- distance
- centre
- vulnerability
- Prior art date
Links
- 238000010304 firing Methods 0.000 abstract 1
- 239000013598 vector Substances 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/34—Direction control systems for self-propelled missiles based on predetermined target position data
- F41G7/343—Direction control systems for self-propelled missiles based on predetermined target position data comparing observed and stored data of target position or of distinctive marks along the path towards the target
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C13/00—Proximity fuzes; Fuzes for remote detonation
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
The missile has a zone tube by which is detects a target at a predetermined distance, towards which it is flying. Equipment in the missile is fed with information covering the target position and/or movement vectors, the missile firing trajectory is simulated together with the ballistic path in order to strike the target, the type and aspect of the target is determined from the missile flight direction, as is a distance between a position for initial zone tube contact between missile and targe and a position for the target vulnerability centre as seen from the flight direction. The distance between the initial zone tube contact position between missile and target and one for the target vulnerability centre is determined based on data obtained from experience concerning the positions for varying target vulnerability centre in relation to the position of the first monitored parts of the target by the missile in flight. The retardation time valid for the distance between the two positions is also determined.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE8605338A SE455816B (en) | 1986-12-11 | 1986-12-11 | Retardation producing appts. for missile |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE8605338A SE455816B (en) | 1986-12-11 | 1986-12-11 | Retardation producing appts. for missile |
Publications (3)
Publication Number | Publication Date |
---|---|
SE8605338D0 true SE8605338D0 (en) | 1986-12-11 |
SE8605338L SE8605338L (en) | 1988-06-12 |
SE455816B SE455816B (en) | 1988-08-08 |
Family
ID=20366602
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE8605338A SE455816B (en) | 1986-12-11 | 1986-12-11 | Retardation producing appts. for missile |
Country Status (1)
Country | Link |
---|---|
SE (1) | SE455816B (en) |
-
1986
- 1986-12-11 SE SE8605338A patent/SE455816B/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
SE8605338L (en) | 1988-06-12 |
SE455816B (en) | 1988-08-08 |
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