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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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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
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Vision app-based Sensor
NXT vegas
Imaging Development Systems GmbH
The app-based system makes it as versatile as a smartphone. With the integrated 1.3 MP CMOS sensor, an integrated liquid lens, LED illumination and a ToF sensor (Time of Flight) for distance measurement, it is fully equipped for many different image processing tasks. As a complete embedded vision component, it simplifies integrated design into custom device hardware and software. The board-level option is also very interesting for OEM equipment manufacturers.
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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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Rapid Evaporative Ionization Mass Spectrometry
REIMS
The innovative iKnife hand-held sampling device produces information-rich vapor directly from the surface of the sample, which when analyzed by a time of flight (Tof) MS, provides analysts with an accurate molecular profile in seconds.
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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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Dual Payload Drone Gimbal
FLIR XT2
The FLIR XT2 integrates a high-resolution FLIR thermal sensor and a 4K visual camera with a leading stabilization and machine intelligence technology to quickly transform aerial data into powerful insights. The advanced thermal sensor provides high sensitivity imaging for infrastructure monitoring, energy inspections, firefighting, search and rescue missions, and more. With a fully-integrated dual payload, professionals can now capture actionable thermal and color visible data in a single flight, saving time, money, and lives.
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Sound Velocity Sensor
miniSVS
The Valeport miniSVS uses digital "time of flight" technology to provide the lowest noise, highest accuracy, best resolution sound velocity data available.
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Pregius Global Shutter CMOS USB3 Camera
Lt-C/M4030
When it comes to aerial imaging systems, size, weight, and power restrictions (also known as SWaP) are the deciding factors. These limitations impact flight time for applications such as, precision agriculture, aerial surveillance, photogrammetry, and aerial inspection. Teledyne Lumenera’s Lt-C/M4030 camera offers excellent imaging performance and provides just the right combination of size and performance for unmanned aerial vehicles (UAVs), and a wide variety of other vision applications.
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Pregius Global Shutter CMOS USB3 Board Level Camera
Lt-C/M4030B
With the caseless design of the Teledyne Lumenera Lt Series Board Level Cameras, the Lt-C/M4030B offers a compact option for OEM solutions. With ease of design in mind, the flat back and side mounted connectors for these cameras can provide a smaller foot-print and shorter cable lengths. This caseless design also reduces the mass of the Lt-C/M4030B camera to 28g which makes it ideal for aerial imaging applications such as, precision agriculture with UAVs. By reducing the overall weight of the vision system, a battery powered vision system can increase its flight time and collect more data.
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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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ARINC 664 Part 7 Test & Simulation Interface for PCI Express
PCIe-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 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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ARINC 664 Part 7 PXI Express Test & Simulation Instrument
PXIe-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 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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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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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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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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MIL-STD-1553 Test & Simulation Instrument for PXI
PXI-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 - Time Synchronization to PXI 10MHz reference clock - Real-Time recording and physical bus replay - PXI trigger generation on 1553 bus events - Initiate BC, RT Simulation and BM Capture on PXI Triggers - 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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Time Domain Reflectometers
HL1100 Series
HYPERLABS HL1100 Series TDR instruments provide high-performance test and measurement capabilities for use in the field or in the lab. These instruments are used for applications such as fault detection in cables and interconnects, impedance characterization, time of flight analysis, water level measurement, and more.
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Ultrasonic Sensing
Ultrasonic sensing is the measurement of the time between an ultrasonic signal being sent and received. The interval between these two signals is typically referred to as time-of-flight (ToF) and depends on the distance the ultrasonic wave travels until it is reflected due to an impedance change and the speed of the ultrasonic wave. The basic equation time = distance / speed can be used to measure fluid level, fluid identification/concentration, flow, or proximity.
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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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Dynamic Data Simulator
LS-70-S
The Lumistar LS-70-S PCI Dynamic Data Simulator allows complex data streams to be generated for evaluation of bit synchronizers and PCM decommutator performance. It can also be used for uplink command generation to vehicles in flight, checkout of complete telemetry links, and playback of archived hard drive data in any format with the appropriate dll. The PCI board is only 7 inches long and contains the dynamic simulator and IRIG Time Code Generator.
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Flight Control System Test Platform
The Flight Control System Test Platform provides a hardware in-the-loop (HIL) closed-loop test environment for dynamic and maintenance testing of Flight Control Systems (FCS) of both commercial and military aircraft. The system simulates control surface activities from multiple combinations of rudder, flaps, elevator, aileron, and engine controls to the FCS. The system delivers repeatable, cost-effective testing in a fraction of the time needed with typical in-house simulation test systems.
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Pregius Global Shutter CMOS USB3 Board Level Camera
Lt-C/M2020B
With this next evolution for Teledyne Lumenera, the Lt Series Board Level Cameras have ports located on the side of the camera for easy access. With the Lt-C/M2020B’s 3.2 megapixel resolution, capturing clear images is simple with frame rates up to 55 fps. Instead of connecting to the back of the camera which would generally mean a longer amount of space required within a design, having connectors on the side allows for the back of these cameras to lie flush against the other components of the device. For example, vision systems in unmanned aerial vehicles (UAVs) can reduce their size and subsequent weight using Lt Series Board Level Cameras, thereby increasing flight time.
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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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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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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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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 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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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.
