Showing results: 121 - 135 of 162 items found.
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UTOR
With every new line of code, the chance of a bug appearing increases. If you don't find and fix that bug immediately, it will get much costlier to fix it in the future. According to IBM Systems Sciences Institute, the cost of fixing bugs after product release is up to 5 times higher than during the design phase, which makes it clear why you should start testing early. As a web application testing company, we are involved in every stage of your product development lifecycle. We help you ensure your app's quality while reducing maintenance costs.
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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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PCIe-FC4 -
Avionics Interface Technologies
Half-size four lane PCIe board - Supports Point-to-Point, Switched Fabric, and Arbitrated Loop topologies - Two independent Fibre Channel ports - Two SFP sockets accept fiber or copper transceivers - Each port supports 1, 2, and 4 Gbps speedsComprehensive decoding of FC-1, FC-2, and Upper Layer Protocol (ULP) frames - Full Error Injection and Detection - IRIG-B Time Code Encoder/Decoder for Data Correlation - In-line Port Configuration for Transparent Analyzer - Supports multiple ULPs including FC-AE-ASM, FC-AE-RDMA, FC-AE-1553, and FC-AV - Compatible with AIT’s fcXplorer GUI Bus Analyzer Software
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VME-429 -
Avionics Interface Technologies
4, 8, 16, 32, or 64 Software Programmable Tx/Rx Channels - Programmable High/Low Speed Operation - Concurrent operation of all Tx/Rx Channels at high data rates - Full Error Injection & Detection - 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++, C#, and .net development - Device driver support: Windows, Linux, & VxWorks (others on request) - Designed for extended temperature operations - 64-bit VME - Interface (VME master & slave capability) - Front Panel and Rear I/O (P2) Available
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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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PC104p-1553 -
Avionics Interface Technologies
Dual redundant, single or dual 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 - Four high voltage (up to 30V) programmable DIO lines - Four trigger LVTTL Trigger I/O lines (2 input / 2 output) - ANSI Application interface supporting C, C++, C#, and .NET development - Device driver support: Windows, Linux, & VxWorks (others on request) - Conformal coating available - Designed for extended temperature operations - PC/104+ specification v2.2 compliant
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VME-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 (others on request) - Designed for extended temperature operations - 64-bit VME Interface (VME master & slave capability) - Front Panel and Rear I/O (P2) Available
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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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MOSTS6 -
Holding Informtest
*MOSTS6 is the first Russian instrument (oscilloscope) with a direct sampling rate (8bit ADC), 5 Gigasemp / s per channel. M-module MOSTs6 is designed to work as a part of information measuring systems based on the VXI bus magister as a digital oscilloscope. The M-module is made in the form of a triple-width mezzanine, is installed on a mezzanine carrier and is connected to it via a local information highway.*MOSTS6 is designed to convert instantaneous voltage values of an electrical signal into a digital code, measure instantaneous voltage values, measure time intervals between two instantaneous voltage values through two independent channels.MOSC6, according to the conditions of use, meets the requirements for measuring instruments of group 3 in accordance with GOST 22261-94.
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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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A2T -
U. S. Digital
The A2T is a single axis, digital gravity angle sensor. The A2T serves as a full 360 range absolute tilt sensing programmable level with either digital or analog output. Internally, a rotary bar coded disk is mounted to a weighted gravity driven wheel. A micro-controller strobes an LED to transfer the bar code image onto an optical linear array, then decodes the position every 2 mSec. Magnetic damping provides fast response and settling time while virtually eliminating overshoot and oscillations. An internal EEPROM stores field programmable parameters such as resolution, zero position, direction swap, and mode. This second generation design virtually eliminates the primary accuracy limitation of first generation inclinometers, which is sitation (hysteresis).
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XMC-429 -
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 - IRIG‐B time code encoder/decoder for data correlation - Conduction-cooling and/or conformal coating available - Designed for extended temperature operations - ANSI Application interfaces supporting C, C++, C#, and .net development - Device driver support: Windows, Linux, and VxWorks (others provided upon request)
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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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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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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
