Author :
Siman, Javier ; Jaquenod, Guillermo ; Mascialino, Hugo
Abstract :
A synthetic aperture radar (SAR) is built around a physical matrix of independent Transmit & Receive Modules (TRM). Each TRM has several parameters to be controlled to attain optimal performance and to compensate production dispersion and operation drift, and for calibration of the complete TR chain. The SAR is an instrument of the SAOCOM Low Earth Orbit satellite, which will be launched on 2010. It has 105 TRM, organized in 21 tiles, each one containing 5 TRM and a redundant controller. This paper presents the project and implementation of the redundant controller, based around a space qualified antifuse FPGA. This device was chosen after evaluation of SRAM, FLASH and antifuse technologies , and special considerations have been taken to reduce components count, minimize power consumption, cost, weight, and improve reliability.
Keywords :
artificial satellites; distributed control; field programmable gate arrays; matrix algebra; radar antennas; synthetic aperture sonar; telecommunication network reliability; FPGA-based transmit-receive distributed controller; L-band antenna; SAR antenna; SRAM; dispersion; low earth orbit satellite; operation drift; physical matrix; synthetic aperture radar; Calibration; Distributed control; Low earth orbit satellites; Optimal control; Production; Receiving antennas; Space technology; Synthetic aperture radar; Transmission line measurements; Transmitting antennas;