Failsafe digital bus to analog protocol converter system

• US 5,377,109 A
• Filed: 07/31/1992
• Issued: 12/27/1994
• Est. Priority Date: 07/31/1992
• Status: Expired due to Fees

• Current Assignee: Marconi Astronics Incorporated
• Original Assignee: Lear Astronics Corporation (BAE Systems Plc)
• Inventors: Baker, John A., Burklund, Wayne E., Edmeads, Robert W., Boe, Otto H., Oster, Melvin G.
• Primary Examiner(s): Teska, Kevin J.
• Assistant Examiner(s): LOUIS JACQUES, JACQUES H
• Application Number:
  US07/923,146
• Time in Patent Office: 879 Days
• Field of Search: 364/424.01, 364/424.02, 364/424.03, 364/424.04, 364/424.05, 364/424.06, 364/551.01, 364/580, 364/481, 340/945
• US Class Current: 701/14
• CPC Class Codes: G05B 9/03 with multiple-channel loop, i.e. redundant control systems
• CPC Class Codes: G05D 1/0077 using redundant signals or controls
• CPC Class Codes: G06F 11/0796 Safety measures, i.e. ensuring safe condition in the event of error, e.g. for controlling element
• CPC Class Codes: G06F 11/2007 using redundant communication media
• CPC Class Codes: G06J 1/00 Hybrid computing arrangements digitally-programmed analogue computers G06G7/06

Abstract

A failsafe avionics interface unit serves as a protocol converter system for translating data for control purposes from a digital communication bus to an analog control channel as an upgrade or interface to an existing analog control system. The avionics interface unit includes digital interface bus logic, a digital data processor module, an analog interface, and a mode selection circuit. Data communicated over the digital interface bus is periodically translated into equivalent analog control signals. For safety purposes, the avionics interface unit ensures the integrity of the system by repetitively looping back or wrapping the digital equivalents of the analog output signals and comparing them to commanded digital control values. The protocol converter system additionally monitors communications over the digital data bus for data continuity. If the difference between a wrapped digital equivalent of an analog output signal and an expected value exceeds tolerable limits or if communication fails, the system disconnects its interface from control using redundant software and hardware and returns control to the analog control system.

Claims

1. A protocol converter system comprising:

a digital interface circuit which is adapted for connection to a digital data bus, the digital interface circuit receiving flight control information from the digital data bus and operating in response to the received flight control information to output at least one first digital flight control signal representing the received flight control information;

an analog interface circuit coupled to receive at least one second digital flight control signal from a digital data processor, the analog interface circuit operating in response to each received second digital flight control signal to generate and output an analog flight control signal commanding an aircraft analog flight control computer to execute a maneuver commanded by the received second digital flight control signal; and

the digital data processor coupled to receive the at least one first digital flight control signal from the digital interface circuit, the digital data processor generating and outputting in response to each received first digital flight control signal one of the at least one second digital flight control signals representing the flight control information represented by the first digital flight control signal.

2. A protocol converter system according to claim 1 wherein the received flight control information represented by each first digital flight control signal is generated by a digital control computer and communicated to the digital interface circuit over the digital data bus.

3. A protocol converter system according to claim 1 wherein the digital data processor generates an alive signal if the digital data processor is properly executing instructions and generates a mode selection signal selecting an analog control signal source to be coupled to the aircraft analog flight control computer;

and further comprising;

a mode selection circuit that is coupled to receive each analog flight control signal generated by the analog interface circuit and to receive at least one second analog flight control signal from an analog avionics computer, said second analog flight control signal being adapted to be coupled to the aircraft analog flight control computer, the mode selection circuit also being coupled to receive the mode selection signal, the mode selection signal responding to the selection signal by selecting either the first or the second outputting the selected analog control signal as a command signal for the aircraft analog flight control computer.

4. A protocol converter system according to claim 3 further comprising:

a fault detection circuit to output a selection override signal to the mode selection circuit upon failing to receive any flight control information generated by the digital mission computer, the mode selection circuit operating in response to the received selection override signal to choose the at least one second analog control signal generated by the analog avionics computer as the source of the second analog control signal that is coupled to the aircraft analog flight control computer.

5. A protocol converter system according to claim 4 wherein the selection override signal is outputted by the fault detection circuit when the digital data processor fails receive any flight control information generated by the digital mission computer.

6. A protocol converter system according to claim 3 further comprising:

a watchdog timer circuit coupled to receive the alive signal generated by the digital data processor, the watchdog timer circuit being coupled to output a clear select signal in response to the watchdog timer circuit failing to receive at least one alive signal, the mode selection circuit operating in response to the received clear select signal by choosing the at last one second analog control signal generated by the analog avionics computer as the source of the second analog control signal that is coupled to the aircraft analog flight control computer.

7. A protocol converter system according to claim 1 further comprising:

at least one additional digital data bus communicating redundant flight control information to and from the digital interface circuit.

8. A protocol converter system according to claim 7 wherein the communication on the digital data bus conforms to MIL-STD-1553B.

9. A protocol converter system according to claim 1 wherein the communication on the digital data bus conforms to MIL-STD-1553B.

10. A protocol converter system according to claim 1 wherein the digital data processor executes instructions contained within read only memory.

11. A protocol converter system according to claim 1 wherein the digital data processor includes alterable memory, stores instructions received from the digital data bus in said alterable memory, and executes instructions from said alterable memory.

12. A protocol converter system according to claim 11 wherein the alterable memory retains its contents in the event of a power interruption.

13. A protocol converter system according to claim 11 wherein the alterable memory loses its contents in the event of a power interruption.

14. A protocol converter system according to claim 1 further comprising:

an analog sample circuit coupled to receive at least one analog wraparound signal provided by the aircraft analog flight control computer, the analog sample circuit converting each received analog wraparound signal to a digital value, the digital data processor receiving and storing each digital value and communicating each digital value to the digital control computer in response to a request received from the digital data bus.

15. A protocol converter system according to claim 14 wherein each of at least one second analog flight control signal generated by an analog avionics computer is adapted to be connected to the analog flight control computer and further comprising:

a mode selection circuit coupled to receive a mode selection signal generated by the digital data processor the mode selection signal selecting an analog control signal source to be coupled to the analog flight control computer by choosing between the at least one first-mentioned analog flight control signal output by the analog interface circuit and the at least one second analog control signal generated by the analog avionics computer.

16. A protocol converter system according to claim 14 wherein the analog sample circuit converts each received analog wraparound signal to a 12-bit digital representation and the digital data processor stores the converted 12-bit representations.

17. A protocol converter system according to claim 1 wherein the system further includes the first-mentioned digital data bus and a second digital data bus, the first-mentioned and the second digital data bus each communicating in conformance with MIL-STD-1553B, and each communicating redundant information from the digital control computer to a digital interface circuit.

18. A protocol converter system according to claim 1 further comprising:

an analog sample circuit coupled to receive at least one analog wraparound signal, the analog sample circuit converting each received analog wraparound signal to a digital value, the digital data processor storing each digital value, comparing each stored digital value to a commanded digital value represented the second digital flight control signal generated by the digital data processor and communicating the result of the comparison to the digital control computer.

19. A protocol converter system according to claim 1 wherein each second digital flight control signal coupled to the analog interface circuit is a 12-bit digital signal.

20. A protocol converter system according to claim 1 wherein the analog interface circuit includes:

a digital to analog converter coupled to receive at least one second digital flight control signal from the digital data processor, the digital to analog converter operating in response to each received second digital flight control signal to generate and output an analog flight control signal commanding an aircraft analog flight control computer to execute a maneuver commanded by the received second digital flight control signal.

21. A protocol converter system according to claim 20 wherein the digital data processor generates a selection signal selecting an analog control signal source to be coupled to the aircraft analog flight control computer;

and further comprising;

a mode selection circuit that is coupled to receive at least one second analog flight control signal from an analog avionics computer, said second analog flight control signal being adapted to be coupled to the aircraft analog flight control computer, the mode selection circuit also being coupled to receive the selection signal, the mode selection circuit responding to the selection signal by selecting either the first or the second analog control signal and outputting the selected analog control signal as a command signal for the aircraft analog flight control computer.

22. A protocol converter system according to claim 21 further comprising:

a fault detection circuit coupled to output a selection override signal to the mode selection circuit, the mode selection circuit operating in response to the received selection override signal by choosing the at least one second analog control signal generated by the analog avionics computer as the source of the second analog control signal that is coupled to the aircraft analog flight control computer.

23. A protocol converter system comprising:

a digital interface circuit which is adapted for connection to a digital data bus, the digital interface circuit receiving from the digital data bus flight control information generated by a digital avionics computer and operating in response to the received flight control information to output at least one first digital flight control signal representing the received flight control information;

an analog interface circuit coupled to receive at least one second digital flight control signal from a digital data processor, the analog interface circuit operating in response to each received second digital flight control signal to generate and output an analog flight control signal commanding an aircraft analog flight control computer to execute a maneuver commanded by the received second digital flight control signal; and

the digital data processor coupled to receive from the digital interface circuit the at least one first digital flight control signal generated by the digital avionics computer, the digital data processor generating and outputting in response to each received first digital flight control signal one of the at least one second digital flight control signals representing the flight control information of the first digital flight control signal.

24. A protocol converter system according to claim 23 wherein the digital data processor generates an alive signal if the digital data processor is properly executing instructions and generates a selection signal selecting an analog control signal source to be coupled to the aircraft analog flight control computer;

and further comprising;

a mode selection circuit that is coupled to receive at least one second analog flight control signal from an analog avionics computer, said second analog flight control signal being adapted to be coupled to the aircraft analog flight control computer, the mode selection circuit also being coupled to receive the selection signal, the mode selection circuit responding to the selection signal by selecting either the first or the second analog control signal and outputting the selected analog control signal as a command signal for the aircraft analog flight control computer.

25. A protocol converter system according to claim 24 further comprising:

a fault detection circuit coupled to output a selection override signal to a mode selection circuit; and

the mode selection circuit operating in response to the received selection override signal and choosing one of the at least one second analog control signal generated by the analog avionics computer as an analog control signal source to be coupled to the aircraft analog flight control computer.

26. A protocol converter system according to claim 25 wherein the selection override signal is outputted by the fault detection circuit when the digital data processor fails to receive any flight control information generated by the digital mission computer.

27. A protocol converter system according to claim 24 further comprising:

a watchdog timer circuit coupled to receive the alive signal generated by digital data processor, the watchdog timer circuit being coupled to output a clear select signal in response to the watchdog timer circuit failing to receive at least one alive signal, the mode selection circuit operating in response to the received clear select signal by choosing the at least one second analog control signal generated by the analog avionics computer as the source of the second analog control signal that is coupled to the aircraft analog flight control computer.

28. A protocol converter system comprising:

a digital interface circuit which is adapted for connection to at least one digital data bus, the digital interface circuit receiving from said digital data bus flight control information generated by a digital avionics computer and operating in response to the received flight control information to output at least one first digital flight control signal representing the received flight control information;

an analog interface circuit coupled to receive at least one second digital flight control signal from a digital data processor, the analog interface circuit operating in response to each received second digital flight control signal to generate and output an analog flight control signal commanding an aircraft analog flight control computer to execute a maneuver commanded by the received second digital flight control signal; and

the digital data processor coupled to receive from the digital interface circuit the at least one first digital flight control signal representing flight control information generated by the digital avionics computer, the digital data processor generating and outputting in response to each received first digital flight control signal one of the at least one second digital flight control signals representing the flight control information represented by the first digital flight control signal.

29. A protocol converter system according to claim 28 wherein the communication on the digital data bus conforms to MIL-STD-1553B.

30. A protocol converter system according to claim 28 wherein the system further includes two digital data buses, each communicating in conformance with MIL-STD-1553B, and each communicating redundant information from the digital avionics computer to the digital interface circuit.

31. A protocol converter system comprising:

a digital interface circuit which is connectable to at least one digital data bus, the digital interface circuit receiving from said digital data bus flight control information generated by a digital avionics computer and operating in response to the received flight control information to output at least one first digital flight control signal representing the received flight control information;

an analog interface circuit coupled to receive at least one second digital flight control signal from a translation circuit, the analog interface circuit operating in response to each received second digital flight control signal to generate and output an analog flight control signal commanding an aircraft analog flight control computer to execute a maneuver commanded by the received second digital flight control signal; and

the translation circuit coupled to receive from the digital interface circuit the at least one first digital flight control signal generated by the digital avionics computer, the translation circuit generating and outputting in response to each received first digital flight control signal one of the at least one second digital flight control signals representing the flight control information represented by the first digital flight control signal.

32. A protocol converter system comprising:

a digital interface circuit which is adapted for coupling to the at least one digital data bus, the digital interface circuit receiving from said digital data bus control and status information generated by a digital computer and operating in response to the received control and status information to output at least one first digital control signal representing the received control and status information;

an analog interface circuit coupled to receive at least one second digital control signal from a translation circuit, the analog interface circuit operating in response to each received second digital flight control signal to generate and output an analog control signal controlling aircraft control surfaces to execute a maneuver commanded by the received second digital control signal; and

the translation circuit coupled to receive from the digital interface circuit the at least one first digital control signal carrying control information generated by the digital computer, the translation circuit generating and outputting in response to each received first digital control signal one of the at least one second digital control signals representing the control information represented by the first digital control signal.

33. A protocol converter system coupled between at least one digital data bus and an aircraft analog flight control computer, the at least one digital data bus communicating with a digital avionics computer, the protocol converter system comprising:

a digital interface circuit which is adapted for connection to the at least one digital data bus, the digital interface circuit receiving from said digital data bus flight control information generated by a digital avionics computer and operating in response to the received flight control information to output at least one first digital flight control signal representing the received flight control information;

an analog interface circuit coupled to receive at least one second digital flight control signal from a digital data processor, the analog interface circuit operating in response to each received second digital flight control signal to generate and output an analog flight control signal commanding an aircraft analog flight control computer to execute a maneuver commanded by the received second digital flight control signal; and

the digital data processor including a nonvolatile memory which stores instructions received from the digital data bus, the digital data processor executing the instructions stored in the nonvolatile memory, the digital data processor being coupled to receive from the digital interface circuit the at least one first digital flight control signal generated by the digital avionics computer, and the digital data processor generating and outputting in response to each received first digital flight control signal one of the at least one second digital flight control signals representing the flight control information represented by the first digital flight control signal.

34. A protocol converter system according to claim 33 wherein the digital data processor further includes an alterable memory, stores instructions received from the digital data bus in said alterable memory, and executes instructions stored in the alterable memory.

35. A protocol converter system coupled between at least one digital data bus and an aircraft analog flight control computer, the at least one digital data bus communicating with a digital avionics computer, the protocol converter system comprising:

a digital interface circuit which is adapted for coupling to the at least one digital data bus, the digital interface circuit receiving over said digital data bus avionics information generated by the digital avionics computer and operating in response to the received avionics information to output at least one first digital flight control signal representing the received flight control information;

an analog interface circuit coupled to receive at least one second digital flight control signal from a digital data processor, the analog interface circuit operating in response to each received second digital flight control signal to generate and output an analog flight control signal commanding an aircraft analog flight control computer to execute a maneuver commanded by the received second digital flight control signal;

the digital data processor coupled to receive from the digital interface circuit the at least one first digital flight control signal carrying the flight control information generated by the digital avionics computer, the digital data processor generating and outputting in response to each received first digital flight control signal one of the at least one second digital flight control signals representing the flight control information of the first received digital flight control signal; and

an analog sample circuit coupled to receive at least one analog wraparound signal provided by the aircraft analog flight control computer and coupled to the digital data processor, the analog sample circuit converting each received analog wraparound signal to a digital value and communicating the digital value to the digital data processor, the digital data processor storing each digital value and communicating each digital value to the digital data bus for communicating to the digital avionics computer in response to a request received from the digital data bus.

36. A protocol converter system according to claim 35 wherein an analog avionics computer generates at least one second analog flight control signal, each of the at least one second analog flight control signal being adapted to be connected to the analog flight control computer and further comprising:

a mode selection circuit coupled to receive a selection signal generated by the digital data processor and operating in response to the received selection signal to select an analog control signal to be coupled to the analog flight control computer, the selected analog control signal being selected from a group of signals including at least the first-mentioned analog flight control signal output by the analog interface circuit and at least one second analog control signal generated by the analog avionics computer.

37. A protocol converter system according to claim 35 wherein the analog sample circuit converts each received analog wraparound signal to a 12-bit digital representation and the digital data processor stores the converted 12-bit representations.

38. An avionics system comprising:

a digital avionics computer which is adapted for connection to at least one digital interface bus, the digital avionics computer communicating digital flight control information and digital status information over the digital interface bus;

a protocol converter system coupled to receive digital flight control information and digital status information from at least one digital interface bus that is adapted for connection to a digital avionics computer, the protocol converter system operating in response to the received digital communications to output at least one analog flight control signal representing the received flight control information; and

a flight control computer coupled to receive at least one analog flight control signal from the protocol converter system and operating in response to each received analog flight control signal to generate an analog command signal commanding a mechanical actuator to execute a commanded maneuver.

39. An avionics system comprising:

at least one digital interface bus;

a digital avionics computer which is adapted for connection to the at least one digital interface bus, said digital interface bus being used by the digital avionics computer to provide digital flight control information and to receive digital representations of analog wraparound signals generated by an aircraft analog flight control computer;

a protocol converter system that is coupled to at least one digital interface bus, the protocol converter system receiving over the digital data bus digital flight control information provided by the digital avionics computer and translating the received digital flight control information into at least one analog flight control signal representing the received digital flight control information; and

the aircraft analog flight control computer coupled to receive at least one analog flight control signal from the protocol converter system, the analog flight computer operating in response to each received analog flight control signal to generate a command signal for a mechanical actuator to execute a commanded maneuver.

40. An avionics system comprising:

at least one digital interface bus;

a digital avionics computer which is coupled to the at least one digital interface bus, the digital avionics computer communicating digital flight control information to the digital interface bus and receiving digital status information from the digital interface bus;

a protocol converter system that is coupled to communicate with the digital avionics computer over the at least one digital interface bus, the protocol converter system receiving digital communications from the digital avionics computer over the digital data bus and translating the received digital communications into at least one analog flight control signal representing the received digital communications, the protocol converter system receiving samples of analog wraparound control signals generated by an aircraft analog flight control computer, storing digital representations of the received analog wraparound control signals, and communicating each stored digital representation of an analog wraparound control signal to the digital avionics computer; and

the aircraft analog flight control computer coupled to receive at least one analog flight control signal from the protocol converter system, the analog flight computer operating in response to each received analog flight control signal to generate and output a command signal for a mechanical actuator that commands an aircraft maneuver.

41. An avionics system according to claim 40 wherein each sampled analog wraparound control signal is sampled and stored as a 12-bit digital representation.

42. An avionics system comprising:

a digital data bus;

a digital avionics computer coupled to communicate over the digital data bus, the digital avionics computer providing digital flight control information and receiving digital representation of analog wraparound signals generated by an aircraft analog flight control computer;

a protocol converter system that is coupled to communicate with the digital avionics computer using the digital data bus, the protocol converter system receiving digital communications from the avionics computer and translating the received digital communications into at least one analog flight control signal representing the received digital communications, the protocol converter system sampling and storing digital representations of analog wraparound control signals generated by the analog flight control computer and communicating upon demand by the digital avionics computer these digital representations of analog wraparound control signals over the digital data bus; and

the aircraft analog flight control computer coupled to receive at least one analog flight control signal from the protocol converter system, the aircraft analog flight computer operating in response to each received analog flight control signal to generate two identical analog flight control signals, wherein the first said analog flight control signal is coupled command a mechanical actuator to execute a commanded maneuver and the second analog flight control signal is the analog wraparound signal that is received by the protocol converter system.

43. An avionics system according to claim 42 wherein the sampled analog wraparound control signals are sampled and stored as 12-bit digital representations.

44. An avionics system according to claim 42 further comprising:

an analog sample circuit coupled to receive at least one analog wraparound signal provided by the aircraft analog flight control computer, the analog sample circuit converting each received analog wraparound signal to a digital value, the protocol converter system receiving and storing each digital value and communicating each digital value to the digital control computer in response to a request received from the digital data bus.

45. An avionics system comprising:

a digital interface circuit which is adapted for connection to a digital data bus, the digital interface circuit receiving flight control information from the digital data bus and operating in response to the received avionic sensor information to output at least one first digital flight control signal representing the received avionic sensor information;

a digital data processor coupled to receive the at least one first digital flight control signal from the digital interface circuit, the digital data processor generating and outputting in response to each received first digital flight control signal one of the at least one second digital flight control signals representing the avionic sensor information represented by the first digital flight control signal; and

an analog interface circuit coupled to receive at least one second digital flight control signal from the digital data processor, the analog interface circuit operating in response to each received second digital flight control signal to generate and output an analog flight control signal commanding an aircraft analog flight control computer to execute a maneuver commanded by the received second digital flight control signal derived by the digital data processor in response to the received avionic sensor information.