Multi core vehicle management system and method

• US 8,948,933 B2
• Filed: 11/15/2011
• Issued: 02/03/2015
• Est. Priority Date: 11/15/2011
• Status: Active Grant

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Corporation
• Inventors: Pangilinan, Lester J., Olsen, John
• Primary Examiner(s): Holloway, Jason
• Application Number:
  US13/296,495
• Publication Number:
  US 20130124015A1
• Time in Patent Office: 1,176 Days
• Field of Search: 701/1, 701/3, 701/4, 701/11, 701/14, 701/120, 340/971, 340/973
• US Class Current: 701/3
• CPC Class Codes: B64C 19/00 Aircraft control not otherwise provided for
• CPC Class Codes: G01C 23/00 Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
• CPC Class Codes: G05D 1/0088 characterized by the autonomous decision making process, e.g. artificial intelligence, predefined behaviours using knowledge based models G06N5/00
• CPC Class Codes: G06F 17/00 Digital computing or data processing equipment or methods, specially adapted for specific functions information retrieval, database structures or file system structures therefor G06F16/00
• CPC Class Codes: G06F 21/84 output devices, e.g. displays or monitors
• CPC Class Codes: G06F 3/0227 Cooperation and interconnection of the input arrangement with other functional units of a computer G06F3/023 - G06F3/037 take precedence
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/003 Flight plan management
• CPC Class Codes: H04B 1/3877 Arrangements for enabling portable transceivers to be used in a fixed position, e.g. cradles or boosters

Abstract

A flight management system (FMS) including a plurality of FMS components that can include a civil FMS component and a tactical FMS component. Each FMS component can have a processor programmed to execute an FMS software product. The FMS can also include a multi core FMS manager configured to control a plurality of flight management systems and coupled to the plurality of FMS components. The multi core FMS manager can include a plurality of FMS managers, each coupled to one of the FMS components, and a platform interface manager coupled to an avionics system. Each FMS manager can be adapted to transmit flight management data to, and to receive flight management data from, the FMS component to which it is coupled. The platform interface manager can be adapted to provide each FMS component access to the avionics system, such that an aircraft operator can control each FMS component via the FMS.

Claims

1. A computer system having a civil flight management system and a tactical flight management system within a dual-core flight management system, said computer system comprising:

a civil flight management system component running a civilian flight management software product;

a tactical flight management system component running a tactical flight management software product; and

a dual core flight management system manager coupled to both the civil flight management system component and the tactical flight management system component, said dual-core flight management system manager comprising;

a civil flight management system manager coupled to said civil flight management system;

a tactical flight management system manager coupled to said tactical flight management system; and

a common platform interface manager coupled to an avionics system,

said civil flight management system manager adapted to transmit civil flight management data to, and receive civil flight management data from, said civil flight management system component,

said tactical flight management system manager adapted to transmit tactical flight management data to, and receive tactical flight management data from, said tactical flight management system component,

said civil flight management system manager and said tactical flight management system manager each being adapted to transmit flight management data to, and to receive flight management data from, the common platform interface manager, and

said common platform interface manager adapted to provide said civil flight management system component and said tactical flight management system component with access to the avionics system, such that an aircraft operator can control each flight management system component via the common platform interface manager,

wherein said civil flight management system component, said tactical flight management system component and said dual-core flight management system manager run on one single board computer, and

said civil flight management system component is temporally and spatially isolated from said tactical flight management system component.

2. The system of claim 1, wherein said civil flight management system component and said tactical flight management system component are independently updateable.

3. The system of claim 1, wherein the civil flight management system component is unclassified and the tactical flight management component is classified.

4. The system of claim 1, wherein said avionics system includes an unclassified transponder.

5. A flight management system comprising:

a plurality of flight management system components, including a civil flight management system component and a tactical flight management system component, each having a processor programmed to execute a flight management software product; and

a multi core flight management system manager configured to control a plurality of flight management systems and being coupled to the plurality of flight management system components, the multi core flight management system manager comprising;

a plurality of flight management system managers, each coupled to one of the plurality of flight management system components; and

a common platform interface manager coupled to an avionics system,

each flight management system manager adapted to transmit flight management data to, and to receive flight management data from, the flight management system component to which the flight management system manager is coupled,

each flight management system manager adapted to transmit flight management data to, and to receive flight management data from, the common platform interface manager, and

the common platform interface manager adapted to provide each flight management system component access to the avionics system, such that an aircraft operator can control each flight management system component via the common platform interface manager.

6. The flight management system of claim 5, wherein the plurality of flight management system components and the multi core flight management system manager execute on a same computer.

7. The flight management system of claim 5, wherein said plurality of flight management system components are each independently updateable.