The Design Proposal Aerospace Electronic Test Equipment Based on Multi-Interface Data Communication

Yan Jun Zhang; Wen Sheng Qiao; Jin Ling Wang

doi:10.4028/www.scientific.net/AMM.336-338.3

Paper Titles

Preface and Organizing Committee

The Design Proposal Aerospace Electronic Test Equipment Based on Multi-Interface Data Communication
p.3

Multi-Time Averaging TDCs Implemented in an Actel Flash-Based FPGA
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Digital Implementation and Simulation of the ZVS Control Scheme
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The Key Problem of Portable Food Traceability Electronic Weigher Design
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The Design of Signal Generator of Electrical Fast Transients Burst
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Design of Conversion Circuit for Intellect Vortex Flow-Meter
p.33

A Magnet-Coupled Piezoelectric Vibration Energy Harvester
p.38

Viscosity and Density Estimation of Ternary Solution Based on Recursive B-Spline Method
p.42

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 336-338The Design Proposal Aerospace Electronic Test...

The Design Proposal Aerospace Electronic Test Equipment Based on Multi-Interface Data Communication

Abstract:

In the background of requirement which apply in aerospace remote measurement electronic equipment, a new requirement for the universal degree to the remote measurement system is proposed. This paper design communicating solutions of the multi-interface device, hardware circuit,FPGA as the core logic controller, coordinating RS-422 interface chip, Ethernet controller W5300,USB-FIFO,FT245 interface chip and other functional modules. The communication equipment has a variety of interfaces; achieve the reliability of transmission of high data rate. This has been applied for engineering practice and improves the efficiency of the design of the remote measurement equipment and maintenance.