Communications: electrical – Aircraft alarm or indicating systems – Potential collision with other aircraft
Patent
1990-05-08
1993-02-09
Ng, Jin F.
Communications: electrical
Aircraft alarm or indicating systems
Potential collision with other aircraft
340975, 364461, G08G 504
Patent
active
051856069
ABSTRACT:
A display for presenting symbolically to an aircraft flight crew the resolution advisory information developed by a Traffic Collision Avoidance System (TCAS) computer aboard an aircraft. The flight display shows a a line symbol representing the artificial horizon, a pitch scale extending perpendicular to said line symbol and indicating pitch angles with reference to said line symbol, and an aircraft reference symbol indicating by its position along said pitch scale the momentaneous aircraft pitch attitude. Furthermore a pitch cue symbol is displayed consisting of a first line segment extending parallel to the artificial horizon and across said pitch scale, said first line segment indicating a limit pitch value processed from the TCAS vertical speed limit ouput, and an area indicator extending below or above said line segment indicating a range of pitch values bounded by said limit pitch value, which range of pitch values has to be avoided by the aircraft flight crew.
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FAA Advisory Circular AC 20-131, Mar. 10, 1988.
"ATA Standard for TCAS II, Displays, Symbology and Controls", ATA-STD-TCAS II/1A, Jun. 15, 1989, Air Transport Association of America.
"Minimum Operational Performance Standards for Traffic Alert and TCAS", RTCA/DO-185, Sep. 23, 1983.
Hultzer Wim J.
Schless Michel M. C.
Verbaarschot Petrus A. A.
Fokker Aircraft B.V.
Ng Jin F.
Swarthout Brent A.
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