Aging Aircraft Sustainment with Non-Standard Engineering

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Aging Aircraft Sustainment with Non-Standard Engineering NDIA 10 th Annual Systems Engineering Conference Hyatt Regency Mission Bay, San Diego, CA October 22-25, 2007 Kendal Hinton 404-407-6042 [email protected] Chris Fowler 404-407-7094 [email protected]

Transcript of Aging Aircraft Sustainment with Non-Standard Engineering

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Aging Aircraft Sustainmentwith Non-Standard Engineering

NDIA 10th Annual Systems Engineering Conference Hyatt Regency Mission Bay, San Diego, CA

October 22-25, 2007

Kendal Hinton404-407-6042

[email protected]

Chris Fowler404-407-7094

[email protected]

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Evolution of Avionics Systems

FROM…

• Single-Function, stand-alone characterized by multiple subsystems

• Connected multiple analog signals using point-to-point wiring, to provide a single function

TO…

• Digital technology for information transfer

• Allowed network sharing of the physical interface

• Reduced number of interconnections within the airframe

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MIL-STD-1553• Result of a cooperative effort between the military

and industry

• Defines the electrical and protocol characteristics for a digital, serial communication standard among systems

• From its initial release in 1973, the standard has been revised and updated to reflect lessons learned from implementation.

• Currently standard version is revision B, Notice 6

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MIL-STD-1553B Notice 6

• Defines the data bus network as a a main bus cable to which stubs are attached and terminals are connected to the stubs

• Voltage waveforms arrive at different terminals with the least amount of distortion

• Major parameters affecting waveform quality are bus length, number of stubs, and locations and lengths of stubs

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A Design-to-Standard Bus

http://www.n-digital.co.jp/Milestek/diagramandtechinf/Mil1553bComp.intro.files/SVS.JPG

SYSTEMSYSTEM SYSTEM

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Non-Standard A/C 1553 WiringAnalysis

LEGACY ISSUES…

• While strides are being made to integrate avionics systems, the physical infrastructures on the target platforms may not be up to the bus standard.

• Installing wiring that conforms to the standard on any legacy system can be costly

POSSIBLE SOLUTION…

• Using non-compliant wiring installed on an aircraft, can systems reliably exchange information over the bus?

• Beneficial to derive and implement an analysis process

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Non-Standard A/C 1553 WiringAnalysis

To ensure…

• Performance

• Maintenance

• Supportability

Plan to…

• Develop Spice Models

• Execute Lab Tests

• Perform SPICE Analysis of Actual A/C Wiring

• Perform Lab Analysis of Actual A/C Wiring

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Existing A/C 1553 Wiring

RG-180

RG-180

RG-180

Matrix Assembly 2(Aft)

Wheel Well DisconnectCircular Connector

TycoConnectors

Adapter

SMAMatrix Assembly 1(Fwd)

+ - -+

F-16C+ Block Diagram

STP

EW System

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Examining Signal Quality on the Bus Network

• GOAL – To transfer voltage waveforms with minimum distortion

• To determine whether or not a network will perform reliably, its characteristics are measured and compared to the requirements of the standard.

• The quality of the waveform is determined by examining it in the following respects:

• Amplitude

• Zero-crossing distortion

• Waveform tailoff

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Test Waveform

PASS 3200

Bus Coupler

S1 S2

Bus Coupler

PASS 3200

O-SCOPEO-SCOPE

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Laboratory MockupCoupler Coupler

PC with PASSAs BC

PC with PASSAs RT

184Circuit

40 ' Twinax 39 ' Coax

10 ' Twinax

10 ' Twinax

Scope

Scope

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Transformer Circuit Solution

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Existing A/C 1553 WiringEW DATA BUS

Transformer Circuit

Terminal (ALQ-184)

RG-180 Cable

To Stations 3, 5, and 7 (F-16C+)To Stations 1 and 11 (A-10)

FORWARD MATRIX ASSEMBLY (BUS COUPLER) AFT MATRIX ASSEMBLY (BUS COUPLER)

EWDAT+ EWDAT-

Connectors, Adapters

RG-180 Cable Shield (Ground)

E+

E-

E+

E-

1:2

93 O1W

EWDAT+

EWDAT+ EWDAT-

Terminator

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Computer Simulation

• Computer Simulation provides an approximation of the quality of the signal that can be achieved with a hardware mockup

• A SPICE program was used to model a transmission line defined by the characteristics of the standard and non-standard wiring

• The transmission line was linked to other components, i.e. resistors and transformers, to form the standard 1553 bus design

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SPICE Bus Configuration

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Impact of Non-Standard Wiring

• BC commands one word transmit from RT (0x0C21 1-T-1-1)

• RT answers with status word followed by 1 data word

• Examine waveform quality (MIL-HDBK-1553, § 40.9)

• Amplitude

• Zero-crossing distortion

• Tailoff

40’ Twinax

39’ Coax

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Input Waveform Amplitude at RT

• Measured Voltage

• Twinax: 5.4 v

• Coax: 3.12 v

• Requirement: 0.86 – 14.0 v

40’ Twinax

39’ Coax

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Input Waveform Zero-Crossing at RT

• Measurement shown is zero-crossing for first bit of command word to the first bit of the data word

• Measured Time

• Twinax: 2.02 μs

• Coax: 2.04 μs

• Requirement: 2 μs ±150 ns

40’ Twinax

39’ Coax

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Input Waveform Tailoff at RT

• Voltage must be less than ±250 mV for the period beginning 2.5 µs following the last mid-bit zero-crossing.

• Both waveforms exhibit clear end to data waveform.

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Impact of Non-Standard Wiring – BC• BC commands 1-word

transmit from RT 1 (0x0C21 1-T-1-1)

• RT 1 answers with status word followed by 1 data word

• Examine waveform quality (MIL-HDBK-1553, § 40.9)• Amplitude

• Zero-crossing distortion

• Tailoff

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Input Waveform Amplitude at BC

• Measured Voltage

• Twinax: 5.28 v

• Coax: 2.82 v

• Requirement: 0.86 – 14.0 v

40’ Twinax

39’ Coax

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Input Waveform Zero-Crossing at BC

• Measurement shown is zero-crossing for first bit of command word to the first bit of the data word

• Measured Time

• Twinax: 2.0 μs

• Coax: 2.06 μs

• Requirement: 2 μs ±150 ns

40’ Twinax

39’ Coax

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Input Waveform Tailoff at BC

• Voltage must be less than ±250 mV for the period beginning 2.5 µs following the last mid-bit zero-crossing.

• Both waveforms exhibit clear end to data waveform.

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Impact of High Traffic Level

• Maximum bus loading was added to the analysis

• Message changed to a 32-word transfer at the minimum inter-message gap, resulting in a bus loading at just over 99%

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Impact of High Traffic Level

• Measured Voltage

• 5.0 v

Input Waveform Amplitude

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Impact of High Traffic Level

• Measured Time

• 1.96 µs

Zero-crossing Deviation

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Impact of High Traffic Level

• The waveform exhibits a clear end to data waveform

Input Waveform Tailoff

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Use of non-standard wiring OK?

• Short answer: Yes.

• What gets “done-to” should be “un-done” at the terminal end.

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Non-Standard A/C 1553 WiringAnalysis

• Sufficient Performance

• Low Maintenance

• Easy Supportability

• Minimal Cost