PL302108A1 - Method of launching and controlling a missile from an aircrafts as well as method of homing it after launching - Google Patents

Method of launching and controlling a missile from an aircrafts as well as method of homing it after launching

Info

Publication number
PL302108A1
PL302108A1 PL94302108A PL30210894A PL302108A1 PL 302108 A1 PL302108 A1 PL 302108A1 PL 94302108 A PL94302108 A PL 94302108A PL 30210894 A PL30210894 A PL 30210894A PL 302108 A1 PL302108 A1 PL 302108A1
Authority
PL
Poland
Prior art keywords
launching
aircrafts
missile
homing
controlling
Prior art date
Application number
PL94302108A
Inventor
Francois Duclos
Didier Lhote
Original Assignee
Sagem
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Sagem filed Critical Sagem
Publication of PL302108A1 publication Critical patent/PL302108A1/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G9/00—Systems for controlling missiles or projectiles, not provided for elsewhere
    • F41G9/02—Systems for controlling missiles or projectiles, not provided for elsewhere for bombing control

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
PL94302108A 1993-02-02 1994-02-01 Method of launching and controlling a missile from an aircrafts as well as method of homing it after launching PL302108A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9301094A FR2701104B1 (en) 1993-02-02 1993-02-02 Method for launching and controlling a projectile from an aircraft and method for guiding it after launch.

Publications (1)

Publication Number Publication Date
PL302108A1 true PL302108A1 (en) 1994-08-08

Family

ID=9443624

Family Applications (1)

Application Number Title Priority Date Filing Date
PL94302108A PL302108A1 (en) 1993-02-02 1994-02-01 Method of launching and controlling a missile from an aircrafts as well as method of homing it after launching

Country Status (7)

Country Link
EP (1) EP0610128B1 (en)
CZ (1) CZ21894A3 (en)
DE (1) DE69404335T2 (en)
ES (1) ES2107142T3 (en)
FR (1) FR2701104B1 (en)
PL (1) PL302108A1 (en)
ZA (1) ZA94638B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19753752C1 (en) * 1997-12-04 1999-07-29 Eurocopter Deutschland Device and method for determining the point of impact of a ballistic missile
FR2870608B1 (en) * 2004-05-18 2006-08-11 Airbus France Sas METHOD AND DEVICE FOR GUIDING AN AIRCRAFT FOR PARACHUTAGE ASSISTANCE

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE327933B (en) * 1969-07-09 1970-08-31 Saab Ab
US4121246A (en) * 1976-09-27 1978-10-17 The Boeing Company Ground impact point prediction system concept for airdrops
FR2681676B1 (en) * 1991-09-24 1993-11-05 Thomson Brandt Armements METHOD FOR WIDENING AMMUNITION WITH A DELAYED BRAKING DEVICE, AND AMMUNITION FOR IMPLEMENTING THE METHOD.
FR2681675B1 (en) * 1991-09-24 1993-11-05 Thomson Brandt Armements METHOD FOR MULTIMODE WIDTH AMMUNITION WITH DEFERRED BRAKE CONTROL, AND AMMUNITION FOR IMPLEMENTING THE METHOD.

Also Published As

Publication number Publication date
EP0610128B1 (en) 1997-07-23
CZ21894A3 (en) 1994-08-17
ES2107142T3 (en) 1997-11-16
FR2701104A1 (en) 1994-08-05
DE69404335T2 (en) 1998-01-29
ZA94638B (en) 1994-09-26
FR2701104B1 (en) 1995-04-07
DE69404335D1 (en) 1997-09-04
EP0610128A1 (en) 1994-08-10

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