Aircraft data instrumentation and acquisition system

• US 4,626,996 A
• Filed: 02/17/1983
• Issued: 12/02/1986
• Est. Priority Date: 02/17/1982
• Status: Expired due to Fees

• Current Assignee: British Aerospace, Inc. (BAE Systems Plc)
• Original Assignee: British Aerospace PLC (BAE Systems Plc)
• Inventors: Arlott, Raymond D. J.
• Primary Examiner(s): Chin, Gary
• Application Number:
  US06/467,367
• Time in Patent Office: 1,384 Days
• Field of Search: 364/550, 364/551, 364/580, 364/424, 364/431.02, 364/431.04, 364/415, 371/20
• US Class Current: 701/14
• CPC Class Codes: G07C 5/085 using electronic data carriers
• CPC Class Codes: H04L 12/403 with centralised control, e.g. polling
• CPC Class Codes: H04L 2012/4028 the transportation system being an aircraft

Abstract

An aircraft data acquisition system, especially a test data system, wherein a central control and acquisition computer receives data from a plurality of remote sub-units each comprising a power supply and a local computer and being connected via a series of input/output modules to respective sets of sensing transducers. Each input/output module comprises a circuit including a series of links which can be made or unmade to adapt the module for driving and/or processing the output of any of a wide variety of transducer types.

Claims

1. A data acquisition system for an aircraft, the system comprising:

a central control and data acquisition computer connected to a digital signal bus and to data recorder means;

a plurality of data acquisition sub-units for being mounted at respective positions distributed about said aircraft and each comprising a local computer, bus interface means connected to said digital signal bus in parallel with the bus interface means of each other sub-units, power supply means, and a plurality of disengageable electrical connector devices each connected to an output of said power supply means, to said local computer and to said bus interface means;

for each data acquisition sub-unit, a plurality of analog signal transducers for sensing respective aircraft operating parameters and, for each transducer, an adaptive transducer interface module, each interface module comprising transducer drive signal supply means connected to the power supply means of the associated data acquisition sub-unit via a respective one of the connector devices of that sub-unit, analog-to-digital conversion and signal holding means connected to the local computer and bus interface means of said associated data acquisition sub-unit via said respective one of the connector devices of that sub-unit, transducer connector terminal means connected to the associated transducer to said transducer drive signal supply means and to said analog-to-digital conversion and signal holding means, first, second, third and fourth pairs of electrically conductive elements, and circuit support means for mounting said pairs with the elements of each pair positioned adjacent one another for having a resistor connected therebetween, said transducer connector terminal means including a first terminal which is connected to one electrically conductive element of each of the first and third pairs thereof, a second terminal which is connected to one electrically conductive element of each of the second and fourth pairs thereof, a third terminal which is connected to the other electrically conductive element of each of the first and second pairs thereof, and a fourth terminal which is connected to the other electrically conductive element of each of the third and fourth pairs thereof;

said drive signal supply means of each interface module being operable for deriving, from the output of the power supply means of said associated data acquisition sub-unit, drive signals for driving the transducer connected to the interface module;

said analog-to-digital conversion and holding means of each interface module being operable, under the control of the local computer of said associated data-acquisition sub-unit, to form and hold digital signals representing samples of the analog signal supplied by the transducer connected to that interface module and to make said held digital signals available to the local computer of said associated data acquisition sub-unit;

each said local computer being operable, under the control of said central control and data acquisition computer, to cause the digital signals made available to it to be transferred in sequence to said central computer via said digital signal bus; and

said central computer being operable to cause said digital signals to be recorded by the data recorder means.

2. A system according to claim 1, wherein the interface modules are operable for sampling all of the transducer signals at the same time and for holding the resultant digital signals;

and the local computers are operable, under the control of the central computer, for transmitting said digital signals in sequence to said digital signal bus.

3. A system according to claim 1, wherein each interface module comprises switch means connected between the power supply means of the associated data acquisition sub-unit and the drive signal supply means of the interface module, the switch means being operable, under the control of the local computer of said associated data acquisition sub-unit, for switching on and off the supply to the drive signal supply means.

4. A system according to claim 1, wherein each interface module comprises controllable frequency filtering means connected to said analog-to-digital conversion and holding means and operable under the control of the local computer of the associated data acquisition sub-unit to selectably control the frequency response to the interface module.

5. A system according to claim 1, wherein each interface module comprises data store means connected to said analog-to-digital conversion and holding means and containing a look-up data table relating actual values of the associated transducer signal with corresponding desired values to be transferred to said central computer.

6. A system according to claim 1, wherein said drive signal supply means of each interface module comprises a fifth and sixth pair of adjacent electrically conductive elements mounted on said circuit support means and respective resistors connected between the elements of each of these pairs, one element of each of these pairs being connected to the power supply means of the associated data acquisition sub-unit and the other element of each of these pairs being connected to a respective terminal of said transducer connector terminal means.

7. A system according to claim 1, wherein each interface module includes a further pair of adjacent electricall conductive elements mounted on said circuit support means, a resistor connected between the elements of said further pair, and switch means connected between one element of said further pair and said drive signal supply means, the other element of said further pair being connected to said analog-to-digital conversion and signal holding means and said switch means being operable, under the control of the local computer of the associated data acquisition sub-unit, for causing a transducer calibration signal to be applied to said analog-to-digital conversion and signal holding means via said further pair of electrically conductive elements and the resistor connected therebetween.

8. A system according to claim 5, wherein said data store means also contains data identifying the associated transducer, the local computer of each data acquisition sub-unit being operable for reading the transducer identifying data from the data store means of each interface module connected to that sub-unit.