FR2326676B1 - - Google Patents
Info
- Publication number
- FR2326676B1 FR2326676B1 FR7628602A FR7628602A FR2326676B1 FR 2326676 B1 FR2326676 B1 FR 2326676B1 FR 7628602 A FR7628602 A FR 7628602A FR 7628602 A FR7628602 A FR 7628602A FR 2326676 B1 FR2326676 B1 FR 2326676B1
- Authority
- FR
- France
- 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
- F41G7/305—Details for spin-stabilized missiles
-
- 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
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)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19752543606 DE2543606C2 (de) | 1975-09-30 | 1975-09-30 | Anordnung zur Flugbahnkorrektur eines rotierenden Geschosses |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2326676A1 FR2326676A1 (fr) | 1977-04-29 |
| FR2326676B1 true FR2326676B1 (enExample) | 1982-04-09 |
Family
ID=5957845
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR7628602A Granted FR2326676A1 (fr) | 1975-09-30 | 1976-09-23 | Procede et dispositif pour augmenter la portee utile des projectiles tires contre des objectifs ponctuels |
Country Status (2)
| Country | Link |
|---|---|
| DE (1) | DE2543606C2 (enExample) |
| FR (1) | FR2326676A1 (enExample) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2658167C2 (de) * | 1976-10-30 | 1983-01-20 | Eltro GmbH, Gesellschaft für Strahlungstechnik, 6900 Heidelberg | Verfahren und Vorrichtung zur Korrektur der Flugbahn eines Geschosses |
| WO1982002765A1 (en) * | 1979-02-21 | 1982-08-19 | Geoffrey Martin Spence | Projectile guidance system |
| EP0058258A1 (en) * | 1981-02-13 | 1982-08-25 | Geoffrey Martin Spence | Projectile guidance system |
| CA1242516A (en) * | 1982-04-21 | 1988-09-27 | William H. Bell | Terminally guided weapon delivery system |
| DE3827764A1 (de) * | 1988-08-16 | 1990-02-22 | Rheinmetall Gmbh | Verfahren zur ermittlung von richtkorrekturwerten |
| DE3904684A1 (de) * | 1989-02-16 | 1990-09-20 | Asea Brown Boveri | Verfahren zur korrektur der flugbahn aus einer rohrwaffe abgefeuerten oder selbststangetriebenen explosivgeschosses sowie geschoss, auf das das verfahren angewendet wird |
| DE3918701A1 (de) * | 1989-06-08 | 1990-12-13 | Diehl Gmbh & Co | Verfahren zur verbesserung der treffgenauigkeit eines programmiert fliegenden flugkoerpers |
| DE4410326C2 (de) * | 1994-03-25 | 1998-07-02 | Rheinmetall Ind Ag | Geschoß mit einer Vorrichtung zur Flugbahnkorrektur |
| DE4416211C2 (de) * | 1994-05-07 | 1996-09-26 | Rheinmetall Ind Gmbh | Verfahren und Vorrichtung zur Flugbahnkorrektur von Geschossen |
| DE4425285C2 (de) * | 1994-07-16 | 1997-04-17 | Rheinmetall Ind Ag | Vorrichtung zur Flugbahnkorrektur von drallstabilisierten Geschossen |
| FR3035205B1 (fr) * | 2015-04-20 | 2018-10-05 | Roxel France | Dispositif de correction de trajectoire d'un projectile et procede de correction de trajectoire |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB524876A (en) * | 1938-02-15 | 1940-08-16 | Sperry Gyrosocope Company Inc | Improvements in or relating to explosive projectiles (such as bombs or aerial torpedoes), and electrical apparatus for controlling their movement during flight |
| US2414103A (en) * | 1941-07-08 | 1947-01-14 | Sperry Gyroscope Co Inc | Apparatus for controlling missiles in flight |
| US2629289A (en) * | 1945-05-03 | 1953-02-24 | Sperry Corp | Fire control apparatus for controlling the flight of missiles |
| US3374967A (en) * | 1949-12-06 | 1968-03-26 | Navy Usa | Course-changing gun-launched missile |
| US3028807A (en) * | 1959-08-24 | 1962-04-10 | Mcdonnell Aircraft Corp | Guidance system |
| US3868883A (en) * | 1964-02-20 | 1975-03-04 | Mc Donnell Douglas Corp | Guidance system |
| CA1009370A (en) * | 1972-01-03 | 1977-04-26 | Ship Systems | Laser guided projectile |
-
1975
- 1975-09-30 DE DE19752543606 patent/DE2543606C2/de not_active Expired
-
1976
- 1976-09-23 FR FR7628602A patent/FR2326676A1/fr active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| DE2543606A1 (de) | 1977-04-07 |
| DE2543606C2 (de) | 1986-11-06 |
| FR2326676A1 (fr) | 1977-04-29 |
Similar Documents
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |