GB1306674A - Method and device for correcting the aim of a weapon - Google Patents
Method and device for correcting the aim of a weaponInfo
- Publication number
- GB1306674A GB1306674A GB1977369A GB1977369A GB1306674A GB 1306674 A GB1306674 A GB 1306674A GB 1977369 A GB1977369 A GB 1977369A GB 1977369 A GB1977369 A GB 1977369A GB 1306674 A GB1306674 A GB 1306674A
- Authority
- GB
- United Kingdom
- Prior art keywords
- telescope
- target
- hairs
- motor
- cross
- 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
- F41G3/00—Aiming or laying means
- F41G3/06—Aiming or laying means with rangefinder
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G5/00—Elevating or traversing control systems for guns
- F41G5/08—Ground-based tracking-systems for aerial targets
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B23/00—Telescopes, e.g. binoculars; Periscopes; Instruments for viewing the inside of hollow bodies; Viewfinders; Optical aiming or sighting devices
- G02B23/14—Viewfinders
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Astronomy & Astrophysics (AREA)
- General Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Telescopes (AREA)
Abstract
1306674 Electric correspondence control systems FRANCE ARMED FORCES MINISTER OF 17 April 1969 [25 April 1968 19773/69 Heading G1N A method of aiming a gun against a movable target consists in following the target with a telescope having cross-hairs displaceable relative to the centre of the telescope field and causing the gun to follow the telescope; measuring the target distance and producing from this measurement and the known speed of the projectile a first signal corresponding to the time necessary for the projectile to reach the target; measuring the angular speed of the gun to produce a second signal; multiplying the first signal by the second signal to obtain a correcting signal; and, using the correction signal to displace the cross-hairs of the telescope away from the centre of the telescope field in a direction opposite to the pursuing direction whereby the gun leads the telescope by an angle which compensates for the movement of the target during flight time of the projectile. As shown in Fig.2 a telescope 20 having movable cross-hairs 17 is trained on a moving target to cause similar movement of a gun turret 21 through a servo-system 22, 23. Members 24, 25 determine the target distance and hence the projectile flight time T, in known manner. A power take-off 7 driven by turret 21 drives the input rotary plate of a ball-type stepup multiplier mechanism 8, at a speed Ko # proportional to the turret speed #. The balls of mechanism 8 are displaced a distance corresponding to time T to produce a mechanical output Ko # T which is applied to the rotor of a synchrogenerator 9 having its stator windings connected to the stator windings of a synchro-motor 10. The generator 9 and motor 10 constitute a Selsyn system and function as divergence detectors. The rotor windings of generator 9 are connected to a reference voltage Uref and the rotor windings of motor 10 are connected to an amplifier 11 connected to a motor-generator reducing unit 12. The mechanical output of unit 12 is connected through a reducing gear 13 to the rotatable stator of motor 10 and through a screw and nut gearing 14 to the cross-hairs 17 and to the displaceable balls of a mechanical integrator 15 similar in construction to the multiplier mechanism 8. The input rotary plate of integrator 15 is driven at constant speed by a motor 16 and the output rotary plate is connected to the rotor of the rotor 10. In a modification the telescope has an additional pair of fixed cross-hairs which are caused to follow the target until the moment of firing when the movable cross-hairs are locked in position and the telescope is moved to align the movable cross-hairs with the target.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR149397 | 1968-04-25 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1306674A true GB1306674A (en) | 1973-02-14 |
Family
ID=8649389
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1977369A Expired GB1306674A (en) | 1968-04-25 | 1969-04-17 | Method and device for correcting the aim of a weapon |
Country Status (3)
Country | Link |
---|---|
US (1) | US3727514A (en) |
FR (1) | FR1605090A (en) |
GB (1) | GB1306674A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8408460B2 (en) | 2010-06-03 | 2013-04-02 | United States Of America As Represented By The Secretary Of The Navy | Auto adjusting ranging device |
CN110345814A (en) * | 2019-06-14 | 2019-10-18 | 上海航天控制技术研究所 | A kind of terminal guidance algorithm not depending on itself target seeker metrical information |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE416583B (en) * | 1976-02-25 | 1981-01-19 | Bofors Ab | VIEW MEASURING DIRECTLY WEAPON |
US4146780A (en) * | 1976-12-17 | 1979-03-27 | Ares, Inc. | Antiaircraft weapons system fire control apparatus |
SE420765B (en) * | 1978-01-18 | 1981-10-26 | Bofors Ab | DEVICE FOR A WEAPON ORIENTATION |
IT1168334B (en) * | 1981-12-03 | 1987-05-20 | Galileo Spa Off | ELECTRONIC CALCULATION EQUIPMENT TO PROVIDE THE DISTANCE OF A LONG POINT A FLIGHT TRAJECTORY, ESPECIALLY THE DISTANCE TO THE CROSS |
GB8920631D0 (en) * | 1989-09-12 | 1990-05-30 | Astra Holdings Plc | Lead computing sight |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2464195A (en) * | 1940-01-04 | 1949-03-08 | Bendix Aviat Corp | Gun sighting device and reflecting means therefor |
US2660794A (en) * | 1942-09-12 | 1953-12-01 | Sperry Corp | Computing gun sight |
CH340736A (en) * | 1955-10-24 | 1959-08-31 | Etat Francais Ministere De La | Gun pointing device |
NO116953B (en) * | 1965-09-06 | 1969-06-09 | Bofors Ab |
-
1968
- 1968-04-25 FR FR1605090D patent/FR1605090A/fr not_active Expired
-
1969
- 1969-04-17 GB GB1977369A patent/GB1306674A/en not_active Expired
- 1969-04-17 US US00817624A patent/US3727514A/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8408460B2 (en) | 2010-06-03 | 2013-04-02 | United States Of America As Represented By The Secretary Of The Navy | Auto adjusting ranging device |
CN110345814A (en) * | 2019-06-14 | 2019-10-18 | 上海航天控制技术研究所 | A kind of terminal guidance algorithm not depending on itself target seeker metrical information |
CN110345814B (en) * | 2019-06-14 | 2021-10-15 | 上海航天控制技术研究所 | Terminal guidance algorithm independent of self seeker measurement information |
Also Published As
Publication number | Publication date |
---|---|
US3727514A (en) | 1973-04-17 |
DE1920992B2 (en) | 1976-04-15 |
DE1920992A1 (en) | 1973-05-03 |
FR1605090A (en) | 1973-01-12 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PLNP | Patent lapsed through nonpayment of renewal fees |