System and method for flight data recording

• US 7,774,112 B2
• Filed: 09/27/2004
• Issued: 08/10/2010
• Est. Priority Date: 09/27/2004
• Status: Active Grant

• Current Assignee: Teledyne Controls, LLC (Teledyne Technologies Incorporated)
• Original Assignee: Teledyne Technologies Incorporated
• Inventors: Nahapetian, Armen
• Primary Examiner(s): Nguyen; Cuong
• Application Number:
  US10/951,005
• Publication Number:
  US 20060069477A1
• Time in Patent Office: 2,143 Days
• Field of Search: 340/436, 340/524, 340/692, 340/870.09, 340/94, 370/412, 370/442, 369 21- 22, 701/3, 701/14, 701/35, 360/5, 123/478
• US Class Current: 701/35
• CPC Class Codes: G07C 5/0808 Diagnosing performance data testing of vehicles G01M17/00; testing of electrical installation on vehicles G01R31/005
• CPC Class Codes: G07C 5/085 using electronic data carriers

Abstract

A method and system for acquiring aircraft parameters that includes sampling an aircraft parameter during a first sampling period, recording the full value of the aircraft parameter sampled during the first sampling period, then sampling the aircraft parameter during a fixed number of subsequent consecutive sampling periods, and recording the change between the value of the aircraft parameter sampled in the subsequent sampling periods and the value of the aircraft parameter sampled in the prior sampling period. A method and system for constructing a data stream that includes merging a voluntary data stream and the mandatory parameters and storing the merged data stream in a flight data recorder while maintaining the certification of the flight data recorder.

Claims

1. A system for acquiring aircraft parameters data, the system comprising:

a data acquisition unit configured to sample an aircraft parameter during a first sampling period; and

sample the aircraft parameter during a plurality of subsequent sampling periods consecutively following the first sampling period; and

a flight data recorder in communication therewith wherein the flight data recorder is configured to record the aircraft parameter'"'"'s full value sampled during the first data period and record a change between the aircraft parameter'"'"'s value sampled in one of the plurality of subsequent sampling period and the aircraft parameter'"'"'s value sampled in a previous sampling period; and

wherein a sampling function of the data acquisition unit is disassociated from a data recording function of the flight data recorder;

wherein the flight data recorder allocates a volume of storage for recording the aircraft parameter over a sampling frame comprising at least one sampling period according to;

B+b(S−

1)

wherein “

S”

is a predetermined number of samples over the sampling frame, “

B”

is a predetermined number of bits for recording the full actual value of the aircraft parameter, and “

b”

is the number of bits required to record the change between the aircraft parameter'"'"'s value in a current sampling period and its value in a previous sampling period, and wherein “

b<

B”

.

2. The system of claim 1, wherein the flight data recorder records a known function representing the change in the aircraft parameter between consecutive sampling periods.

3. The system of claim 1, wherein the flight data recorder records a logarithmic representation of the difference in the aircraft parameter between consecutive sampling periods.

4. The system of claim 1, wherein the plurality of sampling periods comprises a limited and fixed number of subsequent sampling periods.

5. The system of claim 1, wherein the flight data recorder records a difference between a value of the aircraft parameter sampled in a current sampling period and a value of the aircraft parameter sampled in a previous sampling period.

6. The system of claim 1, wherein the flight data recorder allocates a volume of storage for recording the aircraft parameter'"'"'s full value during the first sampling period and the difference between the aircraft parameter'"'"'s value in the first and subsequent sampling periods.

7. The system of claim 1, wherein the flight data recorder records a percentage change in the aircraft parameter between consecutive sampling periods.

8. A system for acquiring aircraft parameters data, the system comprising:

a data acquisition unit to sample an aircraft parameter during a first sampling period; and

sample the aircraft parameter during a plurality of subsequent sampling periods consecutively following the first sampling period; and

a flight data recorder to record the aircraft parameter'"'"'s full value sampled during the first sampling period and, for each of the plurality of subsequent sampling periods, record a change between the aircraft parameter'"'"'s value sampled in subsequent sampling period and the aircraft parameter'"'"'s value sampled in a sampling period immediately preceding the subsequent sampling period.

9. The system of claim 8, wherein the plurality of sampling periods comprises a limited and fixed number of subsequent sampling periods.

10. The system of claim 9, wherein the flight data recorder records a difference between a value of the aircraft parameter sampled in a current sampling period and a value of the aircraft parameter sampled in a previous sampling period.

11. The system of claim 9, wherein the flight data recorder records a percentage change in the aircraft parameter between consecutive sampling periods.

12. The system of claim 9, wherein the flight data recorder records a logarithmic representation of the difference in the aircraft parameter between consecutive sampling periods.

13. The system of claim 9, wherein the flight data recorder records a known function representing the change in the aircraft parameter between consecutive sampling periods.

14. The system of claim 8, wherein the flight data recorder allocates a volume of storage for recording the aircraft parameter'"'"'s full value during the first sampling period and the difference between the aircraft parameter'"'"'s value in the first and subsequent sampling periods.

15. The system of claim 8, wherein the flight data recorder allocates a volume of storage for recording the aircraft parameter over a sampling frame, wherein the sampling frame comprises at least one sampling period.

16. The system of claim 15, wherein the flight data recorder allocates the volume of storage per frame for the aircraft parameter according to:

B+b(S−

1)

wherein “

S”

is a predetermined number of samples over the sampling frame, “

B”

is a predetermined number of bits for recording the full actual value of the aircraft parameter, and “

b”

is the number of bits required to record the change between the aircraft parameter'"'"'s value in a current sampling period and its value in a previous sampling period, and wherein “

b<

B”

.