Alternate destination predictor for aircraft

• US 5,526,265 A
• Filed: 02/14/1995
• Issued: 06/11/1996
• Est. Priority Date: 12/17/1991
• Status: Expired due to Fees

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Nakhla, Nader N. I.
• Primary Examiner(s): PARK, COLLIN
• Application Number:
  US08/388,562
• Time in Patent Office: 483 Days
• Field of Search: 364/428, 364/430, 364/433, 364/434, 364/439, 364/441, 364/442, 364/443, 364/444, 364/446, 364/448, 364/449, 364/458, 244/175, 244/183
• US Class Current: 701/16
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/0039 Modification of a flight plan
• CPC Class Codes: G08G 5/0056 in an emergency situation, e.g. hijacking
• CPC Class Codes: G08G 5/025 Navigation or guidance aids radar or analogous systems specially adapted for landing purposes G01S13/913

Abstract

Disclosed is a flight management computer modification that provides a pilot of an aircraft with a list of alternate landing destinations at which he can land the aircraft in case of an emergency on board or due to some reason why he cannot land at an intended destination. Each of the alternate landing destinations is displayed with data regarding the distance between the aircraft'"'"'s present position and each of the alternate destinations, the estimated time of arrival to fly the aircraft to each of the alternate destinations and an estimate of the fuel remaining on board the aircraft if the aircraft were to land at the alternate destinations. The data allows the pilot to compare the benefits of landing at one of the alternate destinations versus landing at another. The data is calculated assuming a direct flight from the aircraft'"'"'s present position to the alternate as well as assuming a missed approach at the intended destination and a flight from the intended destination to the alternate landing destination. The computational time required to produce the data for the pilot is minimized by increasing the size of the integration steps used by the flight management computer to calculate estimated time of arrival and fuel remaining and by using the flight management computer'"'"'s precalculated values for optimum climb and descent angles.

Claims

1. An aircraft flight management computer system that provides a pilot of the aircraft with information regarding a plurality of alternate landing destinations where the aircraft can be landed, comprising:

a central processing unit that executes a number of program instructions that cause the aircraft flight management computer system to search a navigational data base on board the aircraft to determine a plurality of alternate landing destinations nearest the aircraft'"'"'s present location and to determine a series of data for each of the alternate landing destinations that provides the pilot with a prediction of the distance between the aircraft'"'"'s present location and the location of each of the alternate landing destinations, a trip altitude at which to fly the aircraft to each of the alternate landing destinations, a prediction of the estimated time of arrival to fly from the aircraft'"'"'s present location to each of the alternate landing destinations and a prediction of an amount of fuel remaining in the aircraft upon arrival at each of the alternate landing destinations; and

to allow the pilot to enter an alternate landing destination not included in the navigational data base and, for each alternate landing destination entered, to determine a series of data for each of the alternate landing destinations that provides the pilot with a prediction of the distance between the aircraft'"'"'s present location and the location of each of the alternate landing destinations, a trip altitude at which to fly the aircraft to each of the alternate landing destinations, a prediction of the estimated time of arrival to fly from the aircraft'"'"'s present location to each of the alternate landing destinations and a prediction of an amount of fuel remaining in the aircraft upon arrival at each of the alternate landing destinations.

2. The aircraft flight management computer system of claim 1, wherein the series of data for each of the alternate destinations is determined assuming a direct flight between the aircraft'"'"'s present location and the location of each of the alternate landing destinations.

3. The aircraft flight management computer system of claim 1, wherein the central processing unit executes a number of program instructions that allow a pilot to select

a missed approach option that determines the series of data for each of the alternate landing destinations assuming a missed approach at an intended destination airport.

4. The aircraft flight management computer system of claim 3, further including:

an interface means for allowing the pilot to alter the prediction of the distance between the aircraft'"'"'s present location and the location of the alternate landing destinations, wherein

the prediction of the estimated time of arrival and the prediction of the amount of fuel remaining in the aircraft are redetermined is based on said pilot-altered distance prediction.

5. The aircraft flight management computer system of claim 4, wherein said series of data is determined based on wind conditions.

6. The aircraft flight management computer system of claim 5, wherein said interface also allows the pilot to change the wind conditions on which said series of data is based.