Real-time Monitoring System for Flight Experiment

Performance:
1. Automatic tracking antenna: pitch -5°—90°, azimuth, 0°—360°
2. Process 2 PCM data streams in real time, the rate is less than or equal to 128KW/S
3. Real-time data storage
4. Real-time data transmission
5. Engineering unit conversion, export parameter calculation
6. Limit check and alarm

Front-end equipment performance indicators:
Input signal: 2 PCM data streams
1 channel voice 1 channel video
Output: 16 or 2-way D/A conversion
Fast Ethernet data exchange
Recording: DAT, CD-ROM or HDD
Software Platform: Unix or Windows
Working environment: laboratory environment

use:
It is mainly used for real-time ground monitoring and data processing of aviation flight tests, and can also be used for telemetry and control of targets in the fields of aerospace, navigation, transportation (trains, automobiles), severe weather forecasting, water regime monitoring, storage, and petroleum.