Flight management system

• US 4,774,670 A
• Filed: 04/29/1985
• Issued: 09/27/1988
• Est. Priority Date: 04/29/1985
• Status: Expired due to Fees

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Corporation (Martin Marietta Corporation)
• Inventors: Palmieri, Anthony P.
• Primary Examiner(s): Chin, Gary
• Application Number:
  US06/728,079
• Time in Patent Office: 1,247 Days
• Field of Search: 364/440, 364/443, 364/446, 364/434, 364/424, 244/181, 244/182, 244/183, 244/189, 244/76 R
• US Class Current: 701/204
• CPC Class Codes: G05D 1/101 specially adapted for aircraft

Abstract

An improvement to a Flight Management System (FMS) for an aircraft is described. The improvement comprises: a system coupled to the flight management system for accepting flight data information, including a required time of arrival, and for generating therefrom an estimated arrival time and deriving from the estimated arrival time a signal representative of the required airspeed needed to allow the aircraft to reach a particular point at the required arrival time; and a system for receiving the signal and for generating an output signal for modifying the actual airspeed of the aircraft to correspond to the required airspeed. The signal is derived by applying to the actual airspeed a correctional factor which is a function of the estimated arrival time and the required arrival time. The correctional factor is generated from the ratio of the difference of the estimated arrival time and the required arrival time to the required arrival time. The estimated arrival time is a function of the flight data information which includes the actual airspeed, flight plan data, and wind data. The actual airspeed is incrementally or decrementally modified. The required airspeed is repetitively generated. The output signal is coupled to the aircraft'"'"'s autothrottle to modify the output thereof to attain and to maintain the required airspeed. The system coupled to the flight management system further generates a time flexibility for determining whether the aircraft is capable of reaching the particular point in space at the particular time.

Claims

1. An improvement to a flight management system for modifying the actual airspeed of an aircraft so as to deliver said aircraft to a particular point in space at a required arrival time, said improvement comprising:

means coupled to said flight management system for accepting flight data information, including said required arrival time, actual air speed, flight plan data, and wind data and for repetitively generating therefrom an estimated arrival time and deriving from said estimated arrival time a signal representative of the required airspeed needed to allow said aircraft to reach said particular point at said required arrival time; and

means for receiving said signal representative of said required air speed and for generating an output signal for modifying said actual airspeed of said aircraft to correspond to said required airspeed.

2. The improvement of claim 1 wherein said signal is derived by applying to said actual airspeed a correctional factor which is a function of said estimated arrival time and said required arrival time.

3. The improvement of claim 1 wherein said aircraft has an autothrottle and said means for generating said output signal is coupled to said autothrottle to modify the output thereof to attain and to maintain said required airspeed.

4. The improvement of claim 2 wherein said correctional factor is generated from the ratio of the difference of said estimated arrival time and said required arrival time to said required arrival time.

5. The improvement of claim 1 wherein said flight data information includes the linear distance between waypoints and the curvilinear distance at waypoints and said estimated arrival time is a function of said linear distance between waypoints and said curvilinear distance at waypoints.

6. The improvement of claim 1 wherein said required speed is generated for said aircraft during cruise.

7. The improvement of claim 1 wherein said required airspeed is repetitively generated.

8. The improvement of claim 1 wherein said actual airspeed is incrementally modified.

9. The improvement of claim 1 wherein said actual airspeed is decrementally modified.

10. The improvement of claim 1 further comprising display means for displaying said required arrival time, said required air speed and said actual airspeed coupled to said flight management system.

11. The improvement of claim 1 wherein said aircraft has predetermined operating capabilities and wherein said means coupled to said flight management system further generates a time flexibility signal for determining whether of said aircraft can reach said particular point in space at said required arrival time.

12. The improvement of claim 11 wherein said time flexibility signal comprising the maximum and minimum estimated constraints of said required arrival time within said operating capabilities.