Aircraft flight data display system

• US 4,604,711 A
• Filed: 09/23/1982
• Issued: 08/05/1986
• Est. Priority Date: 07/23/1982
• Status: Expired due to Fees

• Current Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Original Assignee: Sundstrand Data Control, Inc. (Rtx Corporation)
• Inventors: Frost, Wendell, Knudsen, Chris, Nieuwsma, David, Benn, George
• Primary Examiner(s): Heckler, Thomas M.
• Application Number:
  US06/421,743
• Time in Patent Office: 1,412 Days
• Field of Search: 364/200 MS File, 364/900 MS File, 364/424, 364/439, 340/971, 340/973, 340/974, 340/977, 340/978, 340/980, 434/43, 360/5, 360/6, 360/71, 369/21
• US Class Current: 701/14
• 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: G07C 5/0825 using optical means
• CPC Class Codes: G09G 1/06 using single beam tubes G09G1/26, G09G1/28 take precedence, e.g. three-dimensional or perspective representation, rotation or translation of display pattern, hidden lines, shadows G09G1/28 takes precedence; stereoscopic TV-systems, details thereof H04N13/00; oscilloscopes for three-dimensional representation G01R13/206; vectorscopes G01R13/208

Abstract

In order to provide timely aircraft performance data from an aircraft flight data recorder in a useful format, a flight data display system is provided: with a data storage unit; an interface circuit for reformatting flight data from the flight data recorder; a central processor for converting selected portions of the reformatted data into engineering units and storing the converted data into the storage unit; and a video display unit including a keyboard for selecting the desired portions of the reformatted flight data for display on the video display unit. The video display unit provides for the multicolor display of flight data in either graphical form or in a cockpit instrument form on a cathode ray tube.

Claims

1. A system for displaying flight data from an aircraft flight data recorder, comprising:

a data storage unit;

input means, operatively connected to a source of the flight data from the flight data recorder and to said data storage unit, for reformatting and storing the flight data in said data storage unit, said input means including a sync word detector circuit for detecting sync words in the flight data;

processor means, operatively connected to said input means and said data storage unit, for converting selected portions of said reformatted flight data into engineering units and storing said converted flight data in said storage unit; and

a video display unit including a keyboard operatively connected to said processor effective to cause said processor means to select said portion of said reformatted flight data for conversion into engineering units and to display said converted flight data in the form of cockpit instruments.

2. The system of claim 1 wherein said visual display unit includes a cathode ray tube operatively connected to said central processing unit to write a static cockpit display on said cathode ray tube and to display said converted flight data in said static cockpit display.

3. The system of claim 2 wherein said central processing unit is additionally effective to reformat said converted flight data in said data storage unit into flight data display instructions and coordinates and to transmit said flight data display instructions and coordinates to said visual display unit.

4. The system of claim 3 wherein said central processing unit is additionally effective to reformat selected portions of said converted flight data into ASCII format and storing said selected reformatted data in a predetermined location in said data storage unit and to transmit said selected reformatted data from said predetermined location to said visual display unit for display in numerical form in said static cockpit display.

5. The system of claim 2 wherein said central processing unit is responsive to an operator initiated signal from said visual display unit to cause said display of converted flight data to occur at a second rate substantially greater than real time.

6. The system of claim 1 wherein said input means includes a circuit for generating flight data storage addresses in said data storage means.

7. The system of claim 6 wherein said data storage means inlcudes a high-speed random access memory and said addresses represent locations in said high-speed random access memory.

8. The system of claim 1 wherein said processor means performs said conversion of said selected portions of flight data into engineering units while said input means is reformatting and storing the flight data and while said visual display unit is displaying said converted flight data.

9. A system for the direct display of flight data from an aircraft flight data recorder comprising:

data storage means for storing data;

input means, operatively connected to a source of the flight data from the flight data recorder and to said data storage means, for storing flight data that includes sync words in said data storage means;

processor means, operatively connected to said input means and said data storage means, for converting selected portions of the flight data into engineering units in response to one of the sync words while flight data from said source of flight data is being stored in said data storage means; and

display means, operatively connected to said processor means, for displaying said selected portions of flight data converted into engineering units in the form of cockpit instruments.

10. The system of claim 9 wherein said processor includes means for causing said input means to store the flight data in said data storage means.

11. The system of claim 10 wherein said input means includes means for changing the format of the flight data from the aircraft flight data recorder into a format compatable with said data storage means.

12. The system of claim 10 wherein said input means includes detector means for detecting the sync words and generating a sync signal.

13. The system of claim 12 wherein said processor means responds to said sync signal by storing the flight data in a first predetermined location in said data storage means.

14. The system of claim 13 wherein said processor means initiates said conversion of flight data stored in said predetermined location in response to said sync signal.

15. The system of claim 14 wherein said processor includes means for storing said converted portions of flight data in a second predetermined location in said data storage means.

16. The system of claim 9, 10, 11, 12, 13, 14 or 15 wherein said processor means responds to a signal from said display means to initiate storing of the flight data from the source of flight data in said data storage means.

17. A system for the direct display of selected aircraft flight data from an aircraft flight data recorder, comprising:

interface means, operatively connected to the flight data recorder, for receiving serial flight data from the flight data recorder and converting said serial flight data into flight data words;

data storage means for temporarily storing data;

processor means operatively connected to said interface means and said data storage means for;

causing said interface means to receive said serial flight data from the flight data recorder and to convert said serial flight data to said flight data words, storing said flight data words in a first predetermined location in said data storage means, converting selected flight data from said flight data words into scaled flight data, and storing said scaled flight data in a second predetermined location in said data storage means;

detector means for detecting a sync word in said serial flight data and generating a sync signal identifying the sync word detected;

counter means, operatively connected to said processor means, for counting said flight data words and generating an overflow signal indicating that a predetermined number of flight data words have been received and transmitted to said first predetermined location without a sync work being detected;

data overflow means, responsive to said overflow signal, for tentatively identifying said flight data words; and

display means, operatively connected to said processor means, for visually displaying said scaled flight data stored in said second predetermined location in the form of a cockpit instrument array.

18. The system of claim 17 wherein said interface means includes detector means for detecting a sync word in said serial flight data and generating a sync signal identifying the sync word detected and wherein said processor means includes means for initiating said conversion of flight data words into said scaled flight data in responce to said sync dignal.

19. The system of claim 18 wherein said interface means includes means reponsive to said sync signal for directly loading said flight data words into said first predetermined location.

20. The system of claim 19 wherein said processor means includes means responsive to said sync signal for generating an address in said first predetermined location for storing said flight data words in sequence and transmitting said address to said interface means.

21. The system of claim 20 wherein said interface means includes means for transmitting said flight data words to said first predetermined location prior to identifying a sync word.

22. The system of claim 17 wherein said data storage means includes conversion factors stored in a third predetermined location.

23. The system of claim 22 wherein said processor means includes means for extracting predetermined elements of flight data from said first predetermined location and storing said flight data elements in a fourth predetermined location in said data storage means.

24. The system of claim 23 wherein said processor means includes means for calculating said scaled flight data from said flight data elements and said conversion factors and storing said scaled flight data in said second predetermined location.

25. The system of claim 17 wherein said processor means additionally includes means for converting said scaled flight data into a format acceptable to said display means and means for transmitting said converted flight data to said display means.

26. The system of claim 17 wherein said data storage means includes a high speed random access memory and wherein said first and said second predetermined locations are in said high speed random access memory.

27. The system of claim 17 wherein said first predetermined location includes a first and second buffer area and wherein said processor means includes means for loading sequentially said first buffer area and then said second buffer area with said flight data words and means for sequentially loading said first buffer area with flight data words after said second buffer area has been filled with said flight data words.

28. The system of claim 17 wherein said data overflow means generates an address for storing said tentatively identified data in said predetermined location and generates a signal indicating that said tentatively identified data may be in error.

29. A system for the display of flight data derived from an aircraft flight data recorder, comprising:

a source, on the flight data recorder, of raw flight data;

an interface circuit, operatively connected to said source of raw flight data, for reformatting said raw flight data, said interface circuit including a serial to parallel converter circuit for converting serial data to a parallel word format;

a counter circuit, operatively connected to said serial to parallel converter circuit, effective to generate a signal representing the number of bits of said raw flight data received by said serial to parallel converter circuit;

a high-speed random access memory;

a bulk memory containing programmed instructions;

a central processing unit operatively connected to said interface circuit, said high-speed random access memory and said bulk memory, said central unit being programmed;

(1) to cause said interface unit to load reformatted raw flight data into a first predetermined location in said high-speed random access memory;

(2) to convert selected portions of said reformatted raw flight data into engineering units; and

(3) to store said converted flight data in a second predetermined location in said high-speed random access memory; and

a visual display unit, operatively connected to said central processing unit, to display said converted flight data stored in said second predetermined location in the form of a cockpit instrument array.

30. The system of claim 29 wherein said interface circuit includes a data channel controller circuit operatively connected to said counter circuit and said central processing unit effective to store an address of said first predetermined location in random access memory.

31. The system of claim 30 wherein said data channel controller circuit responds to said counter circuit to increment said address for each of said raw flight data words.

32. The system of claim 29 wherein said interface circuit includes a data channel controller circuit operatively connected to said counter circuit and said central processing unit effective to store an address of said first predetermined location in random access memory.

33. The system of claim 32 wherein said interrupt signal causes said central processing unit to transmit one of said addresses to said data channel controller circuit.

34. The system of claim 29 wherein said high-speed random access memory includes conversion tables for use in converting said reformatted raw flight data into said converted flight data.

35. The system of claim 34 wherein said bulk memory includes a parameter data base that includes said conversion tables and said central processing unit is effective to load said conversion tables into said high-speed random access memory in response to a signal from said visual display unit.

36. The system of claim 29 wherein said first predetermined location includes a buffer area which is divided into a predetermined number of subframes.

37. The system of claim 36 wherein said high-speed random access memory includes a counter and said central processor sequentially loads said reformatted raw flight data into each of said subframes, wherein said counter increments for each subframe loaded and wherein said central processing unit in response to said counter loads said reformatted raw flight data into the first of said subframes when the last subframe has been loaded.

38. The system of claim 29 wherein said high-speed random access memory includes an extracted data buffer for storing said selected portions of said reformatted raw flight data.

39. A system for displaying aircraft data from an aircraft flight data recorder comprising:

a source of raw flight data from the flight data recorder;

a visual display unit including a cathode ray tube and a keyboard;

a data storage unit including conversion parameters for a plurality of aircraft types;

processor means, operatively connected to said raw flight data source, said visual display unit and said data storage unit, for storing said raw flight data in said data storage unit, responding to a signal from said keyboard to select a set of conversion parameters from said data storage unit for a specific aircraft type and for converting said raw data to a format suitable for display on said cathode ray tube utilizing said set of conversion parameters; and

means for displaying a cockpit instrument array on said cathode ray tube and means for displaying in real time said converted flight data in said instrument array.

40. The system of claim 39 wherein said processor means includes rate increase means for displaying said converted flight data at a rate substantially greater than real time.

41. The system of claim 40 wherein said rate increase means includes means for reducing the number of said data converted to said format suitable for display.

42. The system of claim 40 wherein said raw flight data is stored in said data storage unit in time subframes and said rate increase means selects predetermined subframes for converting said raw flight data into said format for display.

43. The system of claim 39 wherein said processor means includes means for displaying on said cathode ray tube a static yoke reference line and means for displaying in response to said converted flight data representing control column and wheel data, a position line wherein the position of the control column is represented by up-down movement of said position line with respect to said static yoke line and the wheel position by tilting said position line with respect to said static yoke line.

44. The system of claim 39 wherein selected portions of said instrument array and said converted flight data are displayed in different colors on said cathode ray tube.

45. A system for displaying aircraft data from an aircraft flight data recorder comprising:

a source of raw flight data from the flight data recorder;

a first data storage unit including a high speed random access memory;

a second data storage unit including a bulk memory including a configuration file defining selected flight data for a predetermined aircraft and a parameter data base;

a central processing unit operatively connected to said first and second data storage units effective to cause the sequential loading of blocks of said raw flight data from said raw flight data source into a first predetermined location within said first data storage unit;

to cause a selected number of data conversion parameters from said parameter data base as defined by said configuration file to be loaded in a second predetermined location within said first data storage unit;

to convert selected portions of said raw flight data into engineering units utilizing said selected data conversion parameters and to store said converted flight data in a third predetermined location within said first data storage unit; and

a visual display unit including a cathode ray tube operatively connected to said central processing unit effective to write a static cockpit display on said cathode ray tube and to display said converter flight data in said static cockpit display, said central processing unit being responsive to an operator initiated signal from said visual display unit to cause said conversion of selected raw flight data to occur at a rate substantially greater than real time and wherein said display of converted flight data occurs at a rate substantially greater than real time.

46. The system of claim 45 wherein said central processing unit is additionally effective to reformat said converted flight data in said third predetermined location into flight data display instructions and coordinates and to transmit said flight data display instructions and coordinates to said visual display unit.

47. The system of claim 46 wherein said central processing unit is additionally effective to reformat selected portions of said converted flight data into ASCII format and storing said selected reformatted data in a fourth predetermined location in said first data storage unit and to transmit said selected reformatted data from said fourth predetermined location to said visual display unit for display in numerical form in said static cockpit display.

48. The system of claim 45 wherein said raw flight data source is a magnetic tape unit operatively connected to said central processing unit and wherein said central processing unit is effective to load selected blocks of said raw flight data into said first predetermined location in response to an operator initiated signal from said visual display unit.

49. The system of claim 45, wherein said configuration file includes a first portion defining data to be displayed in a real time configuration and a second portion defining data to be displayed at a second rate substantially greater than real time.

50. The system of claim 45 wherein said central processing unit is effective to cause said visual display unit to display different portions of said static display and said converted flight parameters in different colors.