Global Patent Index - EP 1839009 A2

EP 1839009 A2 20071003 - MISSILE FITTED WITH AN AUTODIRECTOR COMPRISING AN SYNTHESIS APERTURE RADAR ANTENNA AND ASSOCIATED GUIDING METHOD

Title (en)

MISSILE FITTED WITH AN AUTODIRECTOR COMPRISING AN SYNTHESIS APERTURE RADAR ANTENNA AND ASSOCIATED GUIDING METHOD

Title (de)

MIT EINEM ZIELSUCHKOPF AUSGESTATTETES GESCHOSS MIT EINER RADARANTENNE MIT SYNTHETISCHER APERTUR SOWIE ZUGEHÖRIGES LENKVERFAHREN

Title (fr)

MISSILE EQUIPE D'UN AUTODIRECTEUR COMPORTANT UNE ANTENNE DE RADAR A SYNTHESE D'OUVERTURE ET PROCEDE DE GUIDAGE ASSOCIE

Publication

EP 1839009 A2 20071003 (FR)

Application

EP 05825298 A 20051222

Priority

  • EP 2005057117 W 20051222
  • FR 0413713 A 20041222

Abstract (en)

[origin: WO2006067220A2] The invention relates to a missile (1) fitted with an autodirector comprising an aperture synthesis radar antenna (7) having a main direction (70) of detection, characterized in that the antenna is configured in relation to the missile such that the main direction of the antenna is fixed in relation to the missile and offset by a constant angle (ß) in relation to the longitudinal axis (6) of the missile. The invention also relates to an associated method for altitude-controlled guidance of the missile.

IPC 8 full level

F41G 7/22 (2006.01)

CPC (source: EP)

F41G 7/2246 (2013.01); F41G 7/2286 (2013.01); G01S 13/883 (2013.01); G01S 13/9041 (2019.04)

Citation (search report)

See references of WO 2006067220A2

Citation (examination)

Designated contracting state (EPC)

AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR

DOCDB simple family (publication)

FR 2879753 A1 20060623; FR 2879753 B1 20070420; EP 1839009 A2 20071003; WO 2006067220 A2 20060629; WO 2006067220 A3 20060824; WO 2006067220 B1 20061102

DOCDB simple family (application)

FR 0413713 A 20041222; EP 05825298 A 20051222; EP 2005057117 W 20051222