Shortened aircraft holding patterns

Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – Aeronautical vehicle

Reexamination Certificate

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Details

C701S120000, C244S075100, C340S945000

Reexamination Certificate

active

06847866

ABSTRACT:
Methods, apparatus and program product are provided to obtain a shortened holding pattern exit path for an aircraft from its current position (CP) in or entering a holding pattern to an allowed exit point (EP) of the holding pattern. The flight management system (FMS) determines which segment of the holding pattern the aircraft is currently on, i.e., A, B, or C defines in terms of the holding pattern turn points (TP1, TP2, TP3, TP4) and the waypoint (SP) which is symmetrical to the desired EP. The FMS compares the aircraft CP with EP and SP location and directs turns at the appropriate waypoints to give the shortest allowed exit pathway. Both Type I and Type II holding pattern entries are accommodated.

REFERENCES:
patent: 4692869 (1987-09-01), King et al.
patent: 5553387 (1996-09-01), Newcomb
patent: 6167627 (2001-01-01), Wilder et al.
patent: 6246957 (2001-06-01), Barrer et al.
patent: 20020177943 (2002-11-01), Beardsworth
patent: 20020193915 (2002-12-01), Miller
patent: WO02101686 (2002-12-01), None
Panayiotou et al., “A Sample Path Approach for Solving the Ground-Holding Policy Problem in Air Traffic Control”, IEEE Transactions on Control Systems Technology, vol. 9, No. 3, May 2001.

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