A computer system 20 provided in an aircraft 1 includes, as a module of a computer program to be executed, an approach determination section 31 configured to determine whether the aircraft 1 is approaching a landing site. The approach determination section 31 includes, as a condition for determination of approaching, establishment (C1) of one or both of a condition (C11) that a first absolute altitude A1 obtained by an radio altimeter 21 mounted on the aircraft 1 is low relative to a first approach altitude AA1, and a condition (C12) that a second absolute altitude A2 that is obtained by subtracting an altitude AL of the landing site from a pressure altitude Ap determined by a barometric altimeter 22 mounted on the aircraft 1 is low relative to a predetermined second approach altitude AA2.
Computer system for determining approach of aircraft and aircraft
2018-08-14
Patent
Elektronische Ressource
Englisch
IPC: | G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / G01S RADIO DIRECTION-FINDING , Funkpeilung |
COMPUTER SYSTEM DETERMINING AIRCRAFT APPROACH, AND AIRCRAFT
Europäisches Patentamt | 2017
|COMPUTER SYSTEM FOR DETERMINING APPROACH OF AIRCRAFT AND AIRCRAFT
Europäisches Patentamt | 2017
|COMPUTER SYSTEM FOR DETERMINING APPROACH OF AIRCRAFT AND AIRCRAFT
Europäisches Patentamt | 2017
|NTRS | 1984
|