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ARINC 664 Part 7 Test & Simulation Interface for PCI
PCI-C664-V2
Avionics Interface Technologies
Supports IEEE 802.3 10/100/1000 Mbit/s Full-Duplex Ethernet links - Utilizes SFPs to support both copper and optical interfacesSimulates multiple ARINC 664 End Systems - VL traffic shaping and input VL redundancy management - Supports up to 4K Output VLs and 4K Input VLs - Supports up to 16K Sampling & Queuing output message ports and up to 16K input Sampling & Queuing message ports - ARINC 653, UDP, IP protocols managed onboard - IRIG-B time code encoder/decoder - Automatic message sequencing & periodic data generated onboardError Injection including Runt Frames, Short IFG, and Invalid MAC FCS - Device driver support: Windows, Linux, LabVIEW Real-Time (others on request) - Compatible with AIT’s Flight Simulyzer GUI Bus Analyzer Software
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OEM Sound Velocity Sensors
Valeport’s in-house design and manufacture capability mean we can provide customized OEM versions of our “time of flight” sound velocity technology.
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Portable or Stationary Ultrasonic Flowmeter for Liquids
DUC
Two ultrasonic clamp-on transducers are externally mounted on a pipe and produce an acoustic path. The transducers send and receive acoustic signals and their transit times are measured by an electronic flow transmitter. The signal is accelerated by the flow in the forward direction. The return signal is decelerated by the flow in the opposite direction. The difference in time between the two, together with the path length L, can be used to determine the average flow velocity. This principle is known as the acoustic time-of-flight principle.
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ARINC 429 PMC Interface Module
PMC-429
Avionics Interface Technologies
4, 8, 16, or 32 Software Programmable Tx/Rx ChannelsProgrammable High/Low Speed Operation - Concurrent operation of all Tx/Rx Channels at high data rates - Conduction-cooling and/or conformal coating available - Designed for extended temperature operations - Rate-oriented Label Transmission - Label Selective Trigger for Capture/Filtering - IRIG-B Time Code Encoder/Decoder for Data Correlation - ANSI Application Interface supporting C++, C#, and .net DevelopmentDevice Driver Support: Windows, Linux, VxWorks, and other operating system - Compatible with AIT’s Flight Simulyzer GUI Bus Analyzer Software
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SparkFun Distance Sensor Breakout
4 Meter, VL53L1X (Qwiic)
This SparkFun Distance Sensor Breakout utilizes the VL53L1X next generation ToF (Time of Flight) sensor module to give you the highly accurate measurements at long ranges for its size. The VL53L1X from STMicroelectronics uses a VCSEL (Vertical Cavity Surface Emitting Laser) to emit an Infrared laser to time the reflection to the target. That means that you will be able to measure the distance to an object from 40mm to 4m away with millimeter resolution! To make it even easier to get your readings, all communication is enacted exclusively via I2C, utilizing our handy Qwiic system so no soldering is required to connect it to the rest of your system. However, we still have broken out 0.1”-spaced pins in case you prefer to use a breadboard.
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Optical Sensor Test
For optical sensor test Cohu offers a variety of solutions being driven by requirements for tri-temp, parallelism and stimulus spacing. Customized optical stimulus units are integrated into Cohu’s test handling systems. For light detector test, we implement different types of light sources, such as infrared, ambient- and colored light. We offer different solutions for 3D image sensors combining emitter and receiver tests of LiDAR, Time of Flight and Structured Light devices.
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ARINC 429 Test & Simulation Interface for PCI Express
PCIe-C429
Avionics Interface Technologies
4, 8, 16, or 32 Software Programmable Tx/Rx Channels - Programmable High/Low Speed Operation - Concurrent operation of all Tx/Rx Channels at high data rates - Full error injection and detection • Data capture filtering, 100% bus recording, and physical bus replay - Rate-oriented Label Transmission - Label Selective Trigger for Capture/Filtering - IRIG-B time code encoder/decoder with free-wheeling mode - Application Interface supporting C/C++, C# and VB.NET Development - Device driver support: Windows, Linux, LabVIEW Real-Time (others on request) - Compatible with AIT’s Flight Simulyzer GUI Bus Analyzer Software
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Light-to-Digital Proximity Sensors
Renesas' light-to-digital proximity sensors offer low light sensitivity, superior proximity range performance, low power consumption, easy to use simple output algorithm, and an array of other features including intelligent interrupt, sleep modes and Time of Flight (ToF) signal processing.
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MIL-STD-1553 XMC Interface Module
XMC-1553
Avionics Interface Technologies
Dual redundant, single, dual, or quad stream configurations - Transformer & Direct Bus Coupling - Concurrent Bus Controller, 31 Remote Terminals, & Bus Monitor operation - Full error injection and detection - Multi-level trigger for capture and filtering - IRIG-B time code encoder/decoder - Ten high voltage (up to 30V) programmable DIO lines - Real-Time recording and physical bus replay - ANSI Application interface supporting C, C++, C#, and .NET development - Device driver support: Windows, Linux, VxWorks, & LabVIEW Real-Time (others on request) - Conduction-cooling and/or conformal coating availableDesigned for extended temperature operations - x1 Lane PCI Express Host Interface - Rear (P14) and Front Panel Input/Output - Compatible with AIT’s Flight Simulyzer GUI Bus Analyzer Software
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Data Recorder and Playback System
Curtiss-Wright Defense Solutions
The proliferation of sensors in today’s Intelligence, Surveillance and Reconnaissance (ISR) applications has increased the need for recording and playing back multiple channels of high-speed sensor data. Often times these ISR platforms are airborne which present certain environmental requirements that must be met for the system to be flight ready.
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AC Fuel Flow Signal Generator
TA-100
The TA-100 signal generator was designed to facilitate testing of aircraft fuel flow indicators that require two input signals designated as “Drum” and “Impeller”. This generator provides both signals so as to provide a direct interface to the fuel flow indicator under test. The generator also provides switched power out to the unit under test as well as a 5v source for testing the bezel lighting. The original design was built around the requirements for the AMETEK series indicators (pn: 10171 series). This generator simulates a reference and a time delayed signal of appropriate amplitude for an indication of up to 1200pph for the indicator under test. The “PPH Select” switch provides fixed signal delays representing 0, 200, 400, 800, 1000 and 1200pph flow rates respectively, this provides the mechanic with an expedient check of the indicators accuracy. The “PPH Adjust” control allows the mechanic to vary the signal delay throughout the full range and serves as a good method for checking of pointer smoothness from stop to stop. The unit’s front panel also provides test jacks to monitor the “FDR Output” as well as the drum and impeller signals. The TA-100 requires only 28Vdc to operate. This generator provides a very economical approach to any repair facility or flight department as it becomes an alternative to purchasing two bench top signal generators. The TA-100 generator at the very least can provide a simple functional test and eliminate the high cost of exchanging an indicator as a function of troubleshooting the aircraft system.
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SparkFun ToF Range Finder Sensor for VL6180
12785
This is the SparkFun "Time-of-Flight" Range Finder, a sensor board for the VL6180 distance sensor. Unlike most distance sensors that rely on reflected light intensity or reflected angles to determine range, the VL6180 uses a precise clock to measure the time it takes light to bounce back from a surface. This affords the ToF Range Finder and VL6180 a great benefit over other methods because it can be much more accurate and more immune to noise. Does this technology sound familiar? Well it should, it's the same means cellphones use to detect when the caller is holding their phone to their ear.
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ARINC 664 Part 7 XMC Interface Module
XMC-664-V2
Avionics Interface Technologies
Supports IEEE 802.3 10/100/1000 Mbit/s Full-Duplex Ethernet links - Utilizes SFPs to support both copper and optical interfaces - Simulates multiple ARINC 664 End Systems - VL traffic shaping and input VL redundancy management - Supports up to 4K Output VLs and 4K Input VLs - Supports up to 16K Sampling & Queuing output message ports and up to 16K input Sampling & Queuing message ports - ARINC 653, UDP, IP protocols managed onboard - IRIG-B time code encoder/decoder - Automatic message sequencing & periodic data generated onboard - Error Injection including Runt Frames, Short IFG, and Invalid MAC FCSDevice driver support: Windows, Linux, LabVIEW Real-Time (others on request) - Compatible with AIT’s Flight Simulyzer GUI Bus Analyzer Software
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Guided Wave Radar Level Transmitter
2291
The 2291 Guided Wave Radar level transmitter is designed for continuous level measuring of conductive or non-conductive liquids, pulps and solids. The 2291 level gauge operates based on the well-known TDR (Time Domain Reflectometry) principle. Micropulses are sent along a probe guide at the speed of light. As soon as the impulse reaches the surface of the medium, it is reflected back to the electronic module. Level distance is directly proportional to the flight time of the impulse.
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Sound Velocity, Temperature and Pressure for Underwater Vehicles.
UV-SVP
Designed for Underwater Vehicles where space is at a premium, the UV-SVP is based on the Valeport miniSVS. Incorporating Valeport’s class-leading time of flight sound speed sensor, a PRT temperature sensor and a 0.01% pressure sensor in a compact package weighing just 750 grams (in air), the lightweight titanium housing gives a depth rating of 3000m. A wide range (9-30V DC) isolated power supply and RS232 communications complete the package.
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SparkFun ToF Range Finder Breakout for VL6180
12784
This is the SparkFun "Time-of-Flight" Range Finder, a breakout for the VL6180 distance sensor. Unlike most distance sensors that rely reflected light intensity or reflected angles to determine range, the VL6180 uses a precise clock to measure the time it takes light to bounce back from a surface. This affords the ToF Range Finder and VL6180 a great benefit over other methods because it can be much more accurate and more immune to noise. Does this technology sound familiar? Well it should, it's the same means cellphones use to detect when the caller is holding their phone to their ear.
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Data Monitoring System
1S663-001
The 1S663-001 Data Monitoring System was specifically developed for the Cessna Citation X and serves as the primary diagnostic tool for the aircraft?? electronic Logic Modules. The system is FAA certified for airborne operation. Aft compartment and cabin modules can be tested two at a time while remaining in place. The system is also capable of monitoring the fuel quantity system during flight.
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LIDAR & Direct Time of Flight
LIDAR (Light Detection and Ranging) is a sensor technology for remote object detection and ranging, using a light source and receiver. Emitted light pulses hit objects, reflect, and return to the LiDAR sensor system where the receiver detects the returning light pulse.
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One, Two, or Four Dual Redundant Interface MIL-STD-1553A/B Test & Simulation Module for PXI Express
PXIe-1553
Avionics Interface Technologies
1, 2, or 4 dual redundant MIL-STD-1553 bus interfaces Concurrent BC, multiple RT (31), and BM operations Full error injection and detection • Data capture filtering, 100% bus recording, and physical bus replay Multi-level Trigger for Capture/Filtering IRIG-B Time Encoder/Decoder Real-Time Recording and Physical Bus Replay Application interfaces supporting C, C++, C#, and .NET development Device Driver Support for: Windows, Linux, and LabVIEW Real Time (others provided on request) 10 high voltage (up to 30V) programmable DIO lines Flight Simulyzer GUI Analyzer software
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Image Sensor Testing
IP750Ex-HD Family
The IP750EX-HD has been the test platform that has enabled the industry to manufacture high quality CCD and CMOS image sensors, and it is the most economical platform to meet the needs of newer technologies such as Time of Flight (ToF) sensors. When you use a smartphone, high performance digital still camera, or in-home security and surveillance system, these applications have image sensors most likely tested by Teradyne’s IP750ExHD.
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ST VL53L0X Time-of-Flight Range/Distance Sensor
SEN-36003
Highly integrated breakout board for the ST Micro VL53L0X Time of Flight (ToF) range finder sensor, which builds on the absolute ranging technology introduced with the VL6180X. The VL53L0X drops the ambient light sensing capability of it's predecessor for a 10X improvement in absolute ranging capability, bringing the maximum possible range to 2 meters! As a result, this sensor has even more uses in the robotics, cell phone and gesture recognition space. The SEN-36003 includes the VL53L0X IC mounted between two 4-40 sized mounting holes with on board 2.8V LDO and high-speed signal translation to handle interface voltages from 3V to 5V. The board is interfaced via an I2C interface and function pins have been broken out to a 0.1" pin header. All pins are translated to allow interfacing with any microcontroller in the 3V to 5V operating range.
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MIL-STD-1553 USB & LAN Test & Simulation Module
UXI-1553
Avionics Interface Technologies
Dual redundant, single, dual, or quad stream configurationsConcurrent BC, 31 RTs, and BM operations - Physical Bus ReplayFull error injection/detection capabilities - Programmable trigger and capture - Programmable Bus Coupling and Output Voltage Levels - Onboard IRIG-B time code encoder/decoder for Synchronization - Time Synchronization to IEEE 1588 via Ethernet LAN port - 10 Discrete I/O Interfaces (5 Outputs / 5 Inputs) - Operates from a single USB or Ethernet LAN connection - Supports SAE AS4112/4114 protocol testing requirements- Flight Simulyzer™ GUI Analyzer software
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MIL-STD-1553 Test & Simulation Interface for PCI Express
PCIe-C1553
Avionics Interface Technologies
Dual redundant, single, dual or quad stream configurationsSoftware selectable Transformer, Direct, and Bus Stub Coupling Modes - Concurrent Bus Controller, 31 Remote Terminals, & Bus monitor operation - Full error injection and detection - Multi-level triggers for capture and filtering - Ten high voltage (up from 30V) programmable DIO lines - IRIG-B time code encoder/decoder with free-wheeling mode - Real-Time recording and physical bus replay - x1 Lane PCI Express Host Interface (x4 Physical edge connector) - Application interface supporting C, C++, C#, and .NET development - Device driver support: Windows, Linux, LabVIEW Real-Time (others on request) - Compatible with AIT’s Flight Simulyzer GUI Bus Analyzer Software
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MIL-STD-1553 Interface Board
EXC-4000VME/MCH-x / EXC-4000VXI/MCH-x
The EXC-1553VME/MCH and EXC-1553VXI/MCH cards are based on a MIL-STD 1553 certified "Summit" chip used in many flight critical systems. Each dual redundant channel supports both MIL-STD-1553A and MIL-STD 1553B protocols. Up to eight channels may be programmed individually to operate as a Bus Controller, Remote Terminal, Bus Monitor, or Remote Terminal / Concurrent Bus Monitor. The 32 K x 16 of RAM allotted to each channel for the storage of data and control parameters may be updated in real time.
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ARINC 429 Test & Simulation Interface for PCI Express
PCIe-C429X
Avionics Interface Technologies
16, 32, or 64 ARINC 429 Channels (up to 32 Tx & 32 Rx) - Programmable Tx channel output amplitude - Programmable High/Low Speed Operation - Eight (8) Discrete I/O (Four (4) inputs, and four (4) outputs) - Concurrent operation of all Tx/Rx Channels at high data rates - Full error injection and detection - Data capture filtering, 100% bus recording, and physical bus replay - Rate-oriented Label Transmission - Label Selective Trigger for Capture/Filtering - IRIG-B time code encoder/decoder with free-wheeling mode - Application Interface supporting C/C++, C# and VB.NET Development - Device driver support: Windows, Linux, LabVIEW Real-Time (others on request) - Compatible with AIT’s Flight Simulyzer GUI Bus Analyzer Software
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UNMANNED SOLUTIONS
Hermes 450
The Hermes 450 Unmanned Aerial System (UAS) is a highly reliable, mobile and deployable unit with 15 years of service and more than 100,000 hours of flight time. The fully composite, fully operational Hermes 450 may be launched and recovered from both prepared and semi-prepared runways. This medium-size, multi-payload UAS can operate two payloads simultaneously and provide persistent surveillance with endurance in excess of 18 hours and up to 30 hours with the optional external fuel tanks. The Hermes 450 offers high operational versatility for both military and non-military use, with manual or fully autonomous flight capabilities and common, cutting-edge, redundant avionics.
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Compact PCI Multi-function Decommutator
LS-50-cP
The Lumistar LS-50-cP 3U Compact PCI Multi-function PCM Decommutator offers the greatest flexibility in the industry by incorporating up to 10 functions typically encountered in flight test applications in a single 3U Compact-PCI card slot. Five functions are achieved on the main board (PCM Simulator which can also operate as a BERT, PCM Decommutator, IRIG Time CodeReader, IRIG Time Code Generator, and the same 5 functions can be achieved on the LS-55-DB Multi-Function Decom Daughterboard. CVSD Voice Decoding and h.261 Video Decoding are achieved through software.
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Flight Inspection System
CARNAC
Compliant with ICAO, CARNAC Flight Inspection System enables flight inspection of all types of navaids: ILS, MKR, VOR, VHF, DME, Radars, VASI, PAPI, NDB, TACAN, MLS, GNSS procedures, etc. CARNAC is a compact cost saving solution designed to privilege efficiency and high precision avoiding heavy aircraft modifications and decreasing flight inspection time. It features advanced functions such as real-time processing, high-quality flight reports, calibration and remote control of the receivers, modularity, multi-missions and multi-navaids capabilities, automatic flying measurements procedures.
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ST VL6180X Time of Flight Sensor
SEN-36001
Highly integrated breakout board for the ST Micro VL6180X Time of Flight (ToF) range finder sensor. This sensor has many uses in the robotics, cell phone and gesture recognition space. It has two programmable GPIO pins, and most importantly, measures absolute distance up to 100mm. The SEN-36001 includes a VL6180X IC centered between two 4-40 sized mounting holes with onboard 2.8V LDO and voltage translation to handle interface voltages from 3V to 5V. The board is interfaced via an I2C interface and all IC pins have been broken out to a 0.1" pin header. Example code for the Arduino platform is available below and includes code for both the proximity measurement and ambient light sensing capabilities.
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MIL-STD-1553 Test & Simulation Interface for PCI
PCI-C1553
Avionics Interface Technologies
Dual redundant, single, dual or quad stream configurationsSoftware selectable Transformer, Direct, and Bus Stub Coupling Modes - Concurrent Bus Controller, 31 Remote Terminals, & Bus monitor operation - Full error injection and detection - Multi-level triggers for capture and filtering - Ten high voltage (up from 30V) programmable DIO lines - IRIG-B time code encoder/decoder with free-wheeling mode - Real-Time recording and physical bus replay - PCI & PCIx Compatible, 3.3V and 5V OperationApplication interface supporting C, C++, C#, and .NET development - Device driver support: Windows, Linux, LabVIEW Real-Time (others on request) - Compatible with AIT’s Flight Simulyzer GUI Bus Analyzer Software
