Patent ID: 7765036
Filing Date: 2010-07-27
Classification: G01C,G08G

Abstract:
1. A device to construct and secure a low altitude flight path of an aircraft, such that the aircraft closely follows the terrain of the flight path at a predetermined altitude, said device comprising: a first processing unit which has a Design Assurance Level (DAL) C requirement level formed to determine said flight path, using data coming from a first database, wherein said first database, which is qualified according to a Data Processing Assurance Level (DPAL) 2 standard and which includes precalculated performance of the aircraft, configured to provide a first maximum climb gradient flyable by the aircraft, with all of the engines functioning, depending on a plurality of parameters including speed of the aircraft, the performance being saturated on a best climb gradient flyable by the aircraft with one failed engine; and a second processing unit which has a DAL A requirement level and formed in to check the flight path determined by said first processing unit, using data coming from a second database, wherein: said second database, which is qualified according to a DPAL 1 standard and includes precalculated regulation performance of the aircraft, configured to provide a second maximum climb gradient flyable by the aircraft with one failed engine and to do so uniquely for a best gradient speed.