Aircraft display and control system with virtual backplane architecture

• US 5,778,203 A
• Filed: 10/01/1996
• Issued: 07/07/1998
• Est. Priority Date: 10/01/1996
• Status: Expired due to Term

• Current Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Original Assignee: Honeywell (Honeywell International Inc.)
• Inventors: Endrud, Douglas G., Birkedahl, Byron F.
• Primary Examiner(s): Harvey, Jack B.
• Assistant Examiner(s): Seto, Jeffrey K.
• Application Number:
  US08/724,331
• Time in Patent Office: 644 Days
• Field of Search: 395/281, 395/282, 395/306, 395/308, 395/309, 395/280, 364/424.06
• US Class Current: 710/306
• CPC Class Codes: H04L 12/40 Bus networks
• CPC Class Codes: H04L 12/40182 by using a plurality of communication lines
• CPC Class Codes: H04L 12/40195 by using a plurality of nodes
• CPC Class Codes: H04L 2012/4028 the transportation system being an aircraft

Abstract

An aircraft control system improves system flexibility, scalability, redundancy, and separation. The system uses a "virtual backplane" architecture which maximizes system flexibility and scalability and allows easy integration of new functions. The architecture comprises four major elements: processing modules; input and output modules (i.e. I/O modules); database modules; and an aircraft wide system network. Inter module communication occurs via the aircraft wide system network thereby eliminating the need for point to point communication and making modules independent of physical location or what modular units (MUs) they are in. Predetermined periodic and deterministic broadcast techniques improve the safety and communications efficiency of the system.

Claims

1. An aircraft control system for controlling a plurality of aircraft functions, said system comprising:

a) a virtual backplane bus having,

1) a system bus,

2) a plurality of network interface controllers coupled to said system bus, each of said interface controllers capable of synchronizing with other said interface controllers and transmitting and receiving predefined periodic and deterministic data across said system bus, and,

3) a plurality of backplane buses, one of said backplane busses coupled to each of said interface controllers such that all of said predefined periodic and deterministic data is broadcast across said backplane bus;

b) a plurality of modules, each of said modules having,

1) a functional portion, and,

2) a backplane interface coupled with one of said backplane buses and in communication with said network interface controller for transmitting and receiving data across said system bus, said backplane interface having,

a) a receiver portion having access to all said predefined periodic and deterministic data broadcast on said system bus, and,

b) a transmit portion communicating intermodule data from said functional portion to said network interface controller.

2. The aircraft control system according to claim 1 wherein each of said network interface controllers includes a memory for storing a description of said predefined periodic and deterministic data, said description including timing and sequence information for said deterministic data.

3. The aircraft control system according to claim 2 wherein intermodule communications between said modules are accomplished the same regardless of which backplane bus each of said modules are physically coupled to.

4. The aircraft control system according to claim 3 wherein said plurality of modules include,

a) at least one processing module;

b) at least one I/O module; and

,

c) wherein at least one of said processing modules coupled to one of said backplane buses communicates to at least one of said I/O modules which is coupled to another of said backplane buses.

5. The aircraft control system according to claim 4 wherein said plurality of modules includes a data base module.

6. The aircraft control system according to claim 4 further comprising:

a) at least two system buses, and,

b) wherein said network interface controllers include bus switching means for controlling which system bus supplies said predefined periodic and deterministic data to the attached backplane bus.

7. The aircraft control system according to claim 6 wherein,

a) said at least two system buses includes a crosside system bus;

and,

b) wherein the predefined periodic and deterministic data broadcast on said crosside system bus is broadcast on the backplane bus coupled to said network interface controller.

8. The aircraft control system according to claim 6 wherein at least one of said processing modules is physically located in a display head.

9. The aircraft control system according to claim 8 wherein said processing module physically located in a display head provides backup processing functionality for a processing module physically located in a separate modular unit.

10. The aircraft control system according to claim 6 wherein at least one of said I/O modules are physically located proximately to an aircraft system unit said I/O module communicates with thereby reducing wire length between said I/O module and said aircraft system unit.

11. The aircraft control system according to claim 6 wherein at least one of said processors modules provides processing for an aircraft utility function.

12. The aircraft control system according to claim 6 wherein said backplane interface is a shared memory which is shared between the functional portion of said module and the associated network interface controller.

13. The aircraft control system according to claim 5 wherein,

a) at least one I/O module for receiving raw inertial reference data is physically located in a display head, and,

b) at least one processing module for interpreting said inertial reference data is physically located in said display head.

14. An aircraft communications network comprising:

a) a system bus;

b) at least two modular units, each of said modular units having,

1) a network interface controller capable of synchronizing with other said network interface controllers and transmitting and receiving predefined periodic data on said system bus, and,

2) at least one module, each of said modules having an interface portion in communication with said network interface controller capable of transmitting and receiving data such that all intermodule communications are broadcast across said system bus.

15. A method of redundant control of aircraft systems comprising the steps of:

a) providing an aircraft wide virtual backplane network, said network including,

1) a system bus, and,

2) at least two network interface controllers capable of synchronizing with other said network interface controllers and transmitting and receiving predefined periodic data on said system bus;

b) providing at least two modules, each of said modules having a backplane interface portion and a functional portion, said interface portion having a receiver and a transmitter suitable for handling communication between one of said network interface controllers and said module such that all intermodule communications between said modules are broadcast across said system bus.

16. The method of redundant control of aircraft systems according to claim 15 wherein at least two of said modules which are processing modules, each of said processing modules in communication with separate interface controllers and having a redundant functionality such that any of said processing modules can perform said redundant functionality.

17. A method of redundant control of aircraft systems according to claim 15 wherein at least one of said modules is a remote I/O module physically located in close proximity to the aircraft system unit with which said I/O module communicates thereby reducing the length of communications line for communicating between said I/O module and said aircraft system unit.

18. A method of redundant control of aircraft systems according to claim 15 wherein a processing module functionally associated with said remote I/O module is physically separated from said remote I/O module and communicates with said remote I/O module across said system bus.