发明名称 SYSTEME DE PILOTAGE AUTOMATIQUE PARAMETRALE DESTINE A UN AERONEF
摘要 <p>#CMT# #/CMT# The system has a generic software core (39) automatically steering an aircraft (32) and comprising multiple elementary programmable cells. A setting tool of the generic software core transforms an operating need for the system expressed by a configuration file according to a predetermined configuration area in a database (DB) of binary parameters adapted to set the generic software core. Each cell is configured by the database. A loading and storing unit loads and stores the binary parameters in the database of the aircraft. #CMT# : #/CMT# Independent claims are also included for the following: (1) a method for automatically piloting on board an aircraft (2) a method for developing an automatic control system (3) a method for maintaining an automatic control system (4) a program product comprising a set of programs for executing a method for automatically piloting on board an aircraft. #CMT#USE : #/CMT# Automatic control system for an aircraft. #CMT#ADVANTAGE : #/CMT# The setting tool of the generic software core transforms the operating need for the system expressed by the configuration file according to the predetermined configuration area in the database of binary parameters adapted to set the generic software core, so that the configuration allows automatic controlling of operational needs of the aircraft under development or exploitation without configuring additional parts. #CMT#DESCRIPTION OF DRAWINGS : #/CMT# The drawing shows a schematic block diagram of an automatic control system. DB : Database 32 : Aircraft 36 : Acquisition module 37 : Interface module 39 : Generic software core.</p>
申请公布号 FR2989795(B1) 申请公布日期 2015.02.06
申请号 FR20120001201 申请日期 2012.04.24
申请人 THALES 发明人 DEVAUREIX RODOLPHE;BONNAFFOUX ARNAUD;BIRRE JEROME
分类号 G05D1/00 主分类号 G05D1/00
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