Digital flight data recording system

• US 4,470,116 A
• Filed: 08/02/1982
• Issued: 09/04/1984
• Est. Priority Date: 08/02/1982
• Status: Expired due to Term

• Current Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Ratchford, Michael
• Primary Examiner(s): Chin, Gary
• Application Number:
  US06/404,063
• Time in Patent Office: 764 Days
• Field of Search: 364/424, 364/433, 364/900, 360/5, 360/31, 369/21
• US Class Current: 701/35
• CPC Class Codes: G07C 5/0841 Registering performance data recording measured values G01D; information storage G11B

Abstract

A flight data recording system includes a digital flight data recorder (DFDR) and a digital flight data acquisition unit (DFDAU) having a signal processor and nonvolatile memory for storing signals representative of a deterministic flight mode algorithm which defines a generic aircraft flight profile by preselected modes, each mode defining a flight profile operating station, the deterministic flight mode algorithm defining the nominal values of some number of sensed flight data parameters in terms of the sensed values of some number of the remaining other sensed flight parameters. At each such station, the signal processor comparing the actual sensed mandatory flight parameter value with the corresponding determined value to establish sensor accuracy.

Claims

1. The method of verifying the integrity of recorded flight data parameters in a flight data recording system, comprising the steps of:

sensing the actual signal values of each recorded flight data parameter;

defining a deterministic model of an aircraft generic flight schedule having specified flight mode stations sequentially arranged therealong;

specifying optimum values for each recorded flight data parameter in at least one of said flight mode stations;

comparing in each flight mode said recorded parameter optimum value with said recorded parameter actual sensed values; and

providing a parmanent record of each occurrence in which said actual sensed value differs from said optimum value.

2. A flight data system for recording the actual sensed values of flight parameters from a plurality of aircraft sensors at different flight modes of the aircraft flight profile, comprising:

data recording means, for providing nonvolatile recording of signal representations of the sensed flight parameter values; and

data acquisition means, having signal processing means for providing said signal representations to said flight data recording means, and including signal memory means for storing signals;

as characterized by;

said data acquisition means further including test means for performing operational self testing of the flight data system and aircraft sensors, said test means including program means comprising a plurality of program signals stored in said signal memory means and representing a deterministic flight mode algorithm indicative of optimum values of selected flight parameters at different flight modes of the aircraft flight profile, said signal processing means comparing the sensed signal value of each selected flight parameter with the related optimum signal value of said program means for the same flight mode and providing a test failure signal to said signal memory means in response to each difference signal magnitude therebetween.

3. The system of claim 2 wherein said signal memory means stores said test failure signals in a nonvolatile medium.

4. The fight data system of claim 2, wherein said signal processing means, in response to each test failure signal, compares the failed sensed flight parameter signal value of a present flight mode with the recorded sensed signal value of the same flight parameter in a preceding flight mode to provide a sensor test failure signal in response to the presence of substantially equal values for the same sensed parameter in succeeding flight modes.

5. The flight data recording system of claim 2 wherein said program means deterministic flight mode algorithm indicates said optimum values for each selected flight parameter in each flight mode of the aircraft in dependence on the determined relationship of the selected flight parameter to other flight parameters having known values in the same flight mode.

6. The flight data system of claim 5, wherein said optimum values for each selected flight parameter are dependent on other flight parameters having known values which are independent of the related selected flight parameter in the same flight mode.