EP 3239646 A1 20171101 - SYSTEM INTEGRATION
Title (en)
SYSTEM INTEGRATION
Title (de)
SYSTEMINTEGRATION
Title (fr)
INTÉGRATION DE SYSTÈME
Publication
Application
Priority
EP 16275065 A 20160425
Abstract (en)
A method and apparatus for generating, in an aircraft in flight, a feasibility display indicative of the feasibility of a weapon, the method comprising: providing a performance envelope for the weapon; determining, using the performance envelope, configuration data for configuring a generic algorithm; uploading the configuration data to the aircraft; generating feasibility data indicative of the feasibility of a weapon carried on the aircraft successfully engaging a target and/or the feasibility of a weapon carried on the target successfully engaging the aircraft; determining, on board the aircraft, using the same generic algorithm and the uploaded configuration data, one or more test criteria; performing, on board the aircraft, an assessment process including determining whether or not the feasibility data satisfies the one or more test criteria; and, based the assessment, using the feasibility data, generating the feasibility display.
IPC 8 full level
CPC (source: EP)
F41G 7/001 (2013.01); F41G 7/007 (2013.01); F41G 9/002 (2013.01)
Citation (search report)
- [XAI] EP 2600096 A1 20130605 - EADS DEUTSCHLAND GMBH [DE]
- [A] EP 2876401 A1 20150527 - BAE SYSTEMS PLC [GB]
- [A] WO 2008129435 A2 20081030 - ALENIA AERONAUTICA SPA [IT], et al
- [A] CLARK D ET AL: "Common Launch Acceptability Region Task Group", SAE WORLD AVIATION CONGRESS - PROCEEDINGS OF THE 2001 AEROSPACE CONGRESS, SEATTLE, USA, no. 2001-01-2953, 14 October 2001 (2001-10-14), pages 1 - 10, XP002562059
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
Designated extension state (EPC)
BA ME
DOCDB simple family (publication)
DOCDB simple family (application)
EP 16275065 A 20160425