Flight recorder having capability of storing intermediate data

• US 4,510,803 A
• Filed: 12/27/1982
• Issued: 04/16/1985
• Est. Priority Date: 12/27/1982
• Status: Expired due to Fees

• Current Assignee: Allied Corp. (Honeywell International Inc.)
• Original Assignee: Allied Corp. (Honeywell International Inc.)
• Inventors: Perara, Thomas E.
• Primary Examiner(s): Woodiel, Donald O.
• Assistant Examiner(s): Harding, E.
• Application Number:
  US06/453,554
• Time in Patent Office: 841 Days
• Field of Search: 73/178 R, 73/178 T, 73/178 H, 244/194, 244/164, 364/550, 364/551, 364/579, 364/580, 340/27, 340/870.28, 340/870.11
• US Class Current: 73/178.00R
• CPC Class Codes: G07C 5/085 using electronic data carriers

Abstract

A flight recorder (11) for a vehicle such as an airborne vehicle is provided in which various data is recorded, along with on-board time data (from 38) in order to be processed by ground based equipment (13). The on-board time data is synchronized by using a telemetry signal (DT) which is received by a ground based tracking system so that the timing of the events recorded by the flight recorder (11) may be synchronized with the timing of events recorded by the ground based tracking system. This combined data is provided to the ground based equipment (13) in order that the data at (12) obtained on-board the vehicle can be analyzed. By the use of digital techniques, various measurements, such as acceleration and angular rate may be accurately stored and reproduced. This arrangement reduces repeat costs for multiple tests and increases reliability of test data.

Claims

1. Test equipment for a unit under test characterized by:

(a) means for transmitting a discrete telemetry signal associated with the units;

(b) a first component, associated with the unit, for sensing a plurality of conditions, the first component including;

(i) a clock for providing a timing signal,

(ii) a plurality of sensors for providing signals in response to predetermined conditions of the unit under test, and

(iii) memory means for storing the signals in coordination with the timing signal;

(iv) means for supplying an indication of the discrete telemetry signal to the memory means;

(c) tracking means for receiving the discrete telemetry signal and for measuring a real time difference between the transmission of the discrete telemetry signal and a separate event observed to occur with the unit under test;

(d) a second component remotely disposed from the first component for receiving the data from the memory means and for providing an indication of the conditions sensed by the first component, the second component including;

(i) means for receiving said real time measurement, and

(ii) means for correlating the real time measurement with the information stored in the memory means in order to provide an output relating to the unit under test.

2. Apparatus as described in claim 1 further characterized by the first component including:

(a) an accelerometer providing first signals;

(b) an accelerometer output processing instrument connected to the accelerometer and having two modes of operation, whereby in a first mode, the first signals are converted to second signals representative of a background noise level and in a second mode, the accelerometer output processing instrument provides third signals representative of acceleration combined with the background noise level.

3. Apparatus as described in claim 2 further characterized by:

the accelerometer output processing instrument providing the second and third signals by converting the first signals to a voltage signal such that the difference between the voltage signal in the second mode and the voltage signal in the first mode is proportional to acceleration.

4. Apparatus as described in claim 1 further characterized by:

means for converting the second and third signals to frequency variable signals such that the difference between the frequency derived from the third signal and the frequency derived from the second signal is proportional to acceleration.

5. Apparatus as described in claim 2 further characterized by:

the accelerometer output processing instrument including means for converting the second and third signals to frequency variable signals such that the difference between the frequency derived from the third signal and the frequency derived from the second signal is proportional to acceleration.

6. Apparatus as described in claim 2 further characterized by:

(a) the accelerometer output processing instrument including means for converting the second and third signals to frequency variable signals such that the difference between the frequency derived from the third signal and the frequency derived from the second signal is proportional to acceleration; and

(b) the time of change from the first mode to the second mode establishing a zero point with which to determine a total change in velocity by using the third signal.

7. Apparatus as described in claim 1 further characterized by:

the unit under test being an airborne vehicle having a predetermined flight path and the first component being located within the vehicle.

8. Test equipment for a unit under test characterized by:

(a) a first component, associated with the unit, to sense a plurality of conditions, the first component including;

(i) a clock providing a timing signal,

(ii) a plurality of sensors providing signals in response to predetermined conditions,

(iii) means, connected to at least one of the sensors, for providing an analog signal corresponding to the signal from said one of the sensors,

(iv) an analog to digital converter connected to the analog signal means and converting the analog signal into a digital signal,

(v) memory means for storing the digital signal in coordination with the timing signal,

(vi) means connected to the analog to digital converter and the processing means for controlling the analog to digital converter in order to cause the analog to digital converter to provide the digital signal at selected times, and for providing the signal in digital form to the memory means, and

(vii) means for supplying a discrete telemetry signal to the memory means;

(b) tracking means for receiving the distinct telemetry signal and for measuring a real time difference between the transmission of the discrete signal and a separate event occurring with the unit under test; and

(c) a second component for receiving the data from the memory means and providing an indication of the conditions, the second component including;

(i) means for receiving real time measurement, and

(ii) means for correlating the real time measurement and the information stored in the memory means in order to provide an output of data relating to the unit under test.

9. Test equipment as described by claim 8 further characterized by:

(a) the analog signal representing vehicle acceleration; and

(b) the analog to digital converter converting the analog signal to a frequency variable signal.

10. Apparatus as described in claim 8 further characterized by:

the unit under test being an airborne vehicle having a predetermined flight path and the first component being located within the vehicle.

11. Apparatus as described in claim 9 further characterized by:

the unit under test being an airborne vehicle having a predetermined flight path and the first component being located within the vehicle.

12. Apparatus as described in claim 10 further characterized by:

the separate event, occurring with the unit under test, being an observed flight event of the vehicle.

13. Apparatus as described in claim 11 further characterized by:

the separate event, occurring with the unit under test, being an observed flight event of the vehicle.