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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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ARINC 429 Test & Simulation Instrument for PXI
PXI-C429
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 - 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 - Time Synchronization to PXI 10MHz reference clock - 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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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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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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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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SparkFun Distance Sensor
1.3 Meter, VL53L4CD (Qwiic)
This SparkFun Distance Sensor Breakout utilizes the VL53L4CD next generation ToF (Time of Flight) sensor module to give you the highly accurate measurements at short ranges for its size. The VL53L4CD 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 1mm to 1300mm 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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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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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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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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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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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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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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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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Innovative Multiple - Object Tracking Radar
iMOTR
We have advanced the multiple-object tracking radar concept with an innovative application to meet today’s test range needs. The iMOTR features enhanced clutter suppression capabilities to deliver clearer, more accurate assessments of object launch trajectory and flight path data on airborne and low flying objects. This tracking information can then be handed-off to other radars or data collection sensors in real-time. The system is also better equipped to provide precision time, space, and position information (TSPI) data of multiple objects in flight over a wider field of regard than the current test range radars in service.
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ARINC 429 Test & Simulation Interface for PCI
PCI-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/FilteringIRIG-B time code encoder/decoder with free-wheeling modeApplication Interface supporting C/C++, C# and VB.NET Development - Device driver support: Windows, Linux (others on request) - Compatible with AIT’s Flight Simulyzer GUI Bus Analyzer Software
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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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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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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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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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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 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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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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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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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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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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MIL-STD-1553 PMC Interface Module
PMC-1553
Avionics Interface Technologies
Dual redundant, single, dual, or quad stream configurationsTransformer & 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 available - Designed for extended temperature operations - 3.3v PMC (with 5V Tolerant I/O), 64-bit 33/66MHz - Rear (P14) and Front Panel Input/Output - Compatible with AIT’s Flight Simulyzer GUI Bus Analyzer Software
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Electronic Tachometers
1 1/4″, 2 1/4″ & 3 1/8″ Aircore Propeller tach for Rotax912/914 engines, connects to tach coil, calibrated to Propeller RPM, not Engine RPM! Custom color marking available, internal light optional! Hourmeter can be set to count engine time or flight time and preset to any numbers —(must be done at UMA facility)!—Standard setting 800rpm & above. White or Antique yellow dial with black numbers available, per request!
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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.
