Real-time Monitoring System for Flight Experiment
SKU: MD-P00499·UAV Platforms·Sur commande
Vue d'ensemble
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.
Spécifications techniques
Specifications. Caractéristiques principales : 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.
Spécifications techniques — 1 groups
Caractéristiques principales : 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.
Spécifications techniques
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