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Real-time Monitoring System for Flight Experiment

SKU: MD-P00499·UAV Platforms·Под заказ

Real-time Monitoring System for Flight Experiment
Real-time Monitoring System for Flight Experiment
Real-time Monitoring System for Flight Experiment

Обзор

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 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 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.

Технические характеристики

Specifications. Основные характеристики: Automatic tracking antenna pitch -5 90 , azimuth, 0 360, Input signal 2 PCM data streams, Output 16 or 2-way D/A conversion, Recording DAT, CD-ROM or HDD, Software Platform Unix or Windows, Working environment laboratory environment.

Технические характеристики — 1 groups
Основные характеристики: Automatic tracking antenna pitch -5 90 , azimuth, 0 360, Input signal 2 PCM data streams, Output 16 or 2-way D/A conversion, Recording DAT, CD-ROM or HDD, Software Platform Unix or Windows, Working environment laboratory environment.

Технические характеристики

Specifications

Automatic tracking antenna
pitch -5 90 , azimuth, 0 360
Input signal
2 PCM data streams
Output
16 or 2-way D/A conversion
Recording
DAT, CD-ROM or HDD
Software Platform
Unix or Windows
Working environment
laboratory environment

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