DocumentCode
2655591
Title
Airborne shock response spectra analyzer based on FPGA
Author
Chen De-Rong ; Xiang-bin, Li
Author_Institution
Dept. of Electron. Eng., Tsinghua Univ., Beijing, China
fYear
2003
fDate
25-29 Aug. 2003
Firstpage
224
Lastpage
227
Abstract
How to get enough shock environment information with limited system capacity is a key problem in space vehicle telemetry. In this paper, an airborne shock response spectra analyzer is developed based on FPGA which can real time calculate peak response spectra on board and then sending it to the ground station instead of the signal form three-axis accelerometer during the flight test. Flight test shows the analyzer can effectively compress the shock data and get enough shock environment information with limited system capacity. Moreover, the compression ratio of shock data can be flexibly adjusted according to the telemetry system capacity and real-time requirement of measurement, and some design parameters can be changed on-line. Therefore the analyzer has good applicability.
Keywords
aerospace testing; field programmable gate arrays; shock waves; space telemetry; spectral analysers; FPGA; airborne shock response spectra analyzer; field programmable gate arrays; flight test; limited system capacity; on board spectra; shock data; shock environment information; space vehicle telemetry; three axis accelerometer; Accelerometers; Electric shock; Field programmable gate arrays; Information analysis; Real time systems; Satellite ground stations; Signal analysis; Space vehicles; System testing; Telemetry;
fLanguage
English
Publisher
ieee
Conference_Titel
Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on
Print_ISBN
0-7803-8149-1
Type
conf
DOI
10.1109/ICIASF.2003.1274871
Filename
1274871
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