Abstract
In the aerospace engineering, before the rocket launch, we need to simulate the actual process to collect and store data. This article describes a high-speed data acquisition and storage systems based on the LVDS interface and two-plane flash-operating way. When receiving the simulated rocket ignition signal, the recorder assembled in the rocket records the sensor parameters of various key parts of the rocket high-speedly in the two-plane way; the control center, via the LVDS interface and the USB bus of the integrated test bench, monitors the state parameters in real time.
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