EP 0033283 B1 19860122 - SIMPLIFIED SELF-STEERING SYSTEM FOR A MISSILE SUCH AS A SHELL OR ROCKET
Title (en)
SIMPLIFIED SELF-STEERING SYSTEM FOR A MISSILE SUCH AS A SHELL OR ROCKET
Publication
Application
Priority
FR 8001869 A 19800129
Abstract (en)
[origin: US4397430A] The simplified homing system comprises an accelerometric device mounted directly on the missile structure and associated with discriminating means for delivering signals representative of the lateral acceleration gamma ext of the missle due to outside forces and the centrifugal acceleration gamma c due to the rolling; target detection means directly mounted on the missile structure; passive means ensuring the keeping up of the rolling movement of the missile; means for determining from information supplied by the accelerometric device and discriminating means and by target detection means the serviceable values related to the vector V indicating the relative speed of the missile with respect to the air in a reference system related to the missile and to the vector uc representing the direction of the target with respect to the axis of the missile and means for elaborating a guiding force Fp from the said predetermined serviceable values related to the vectors V and uc.
IPC 1-7
IPC 8 full level
F41G 7/20 (2006.01); F41G 7/22 (2006.01); G05D 1/12 (2006.01)
CPC (source: EP US)
F41G 7/222 (2013.01 - EP US); F41G 7/2253 (2013.01 - EP US); F41G 7/2293 (2013.01 - EP US)
Designated contracting state (EPC)
DE GB IT SE
DOCDB simple family (publication)
EP 0033283 A2 19810805; EP 0033283 A3 19811202; EP 0033283 B1 19860122; DE 3173544 D1 19860306; FR 2474686 A1 19810731; FR 2474686 B1 19860404; JP S5757313 A 19820406; US 4397430 A 19830809
DOCDB simple family (application)
EP 81400119 A 19810128; DE 3173544 T 19810128; FR 8001869 A 19800129; JP 1218281 A 19810129; US 23011781 A 19810126