FR2597226B3 - GUIDANCE COMPUTER FOR A LAUNCHING INSTALLATION - Google Patents
GUIDANCE COMPUTER FOR A LAUNCHING INSTALLATIONInfo
- Publication number
- FR2597226B3 FR2597226B3 FR8704506A FR8704506A FR2597226B3 FR 2597226 B3 FR2597226 B3 FR 2597226B3 FR 8704506 A FR8704506 A FR 8704506A FR 8704506 A FR8704506 A FR 8704506A FR 2597226 B3 FR2597226 B3 FR 2597226B3
- Authority
- FR
- France
- Prior art keywords
- guidance computer
- launching installation
- launching
- installation
- guidance
- 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
- F41G5/00—Elevating or traversing control systems for guns
- F41G5/14—Elevating or traversing control systems for guns for vehicle-borne guns
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/007—Preparatory measures taken before the launching of the guided missiles
-
- 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
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3611904 | 1986-04-09 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2597226A1 FR2597226A1 (en) | 1987-10-16 |
FR2597226B3 true FR2597226B3 (en) | 1988-05-20 |
Family
ID=6298294
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8704506A Expired FR2597226B3 (en) | 1986-04-09 | 1987-03-31 | GUIDANCE COMPUTER FOR A LAUNCHING INSTALLATION |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2597226B3 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2574561B2 (en) | 1990-08-16 | 1997-01-22 | エイチイー・ホールディングス・インコーポレーテッド・ディービーエー・ヒューズ・エレクトロニクス | Missile interface unit |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3802894A1 (en) * | 1988-02-01 | 1989-08-10 | Esg Elektronik System Gmbh | FIRE CONTROL SYSTEM |
US5118050A (en) * | 1989-12-07 | 1992-06-02 | Hughes Aircraft Company | Launcher control system |
FR2908219A1 (en) * | 2006-11-07 | 2008-05-09 | Airbus France Sas | Aircraft e.g. civilian cargo airplane, guiding device, has guiding unit provided with aircraft guiding rules, and processing all guiding controls of aircraft irrespective of guiding modes, where controls are transmitted to activation unit |
-
1987
- 1987-03-31 FR FR8704506A patent/FR2597226B3/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2574561B2 (en) | 1990-08-16 | 1997-01-22 | エイチイー・ホールディングス・インコーポレーテッド・ディービーエー・ヒューズ・エレクトロニクス | Missile interface unit |
Also Published As
Publication number | Publication date |
---|---|
FR2597226A1 (en) | 1987-10-16 |
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