Here is a client’s demand for L S band 100Mbps 200km 2x20WPA drone video data transceiver.
Requirment:
L and S band
2x20w PA
2 input LAN (RJ45)
1 RS232 input (hai chiều)
Airborne design
Datarate: 100 Mb/giây
Max Range: 200km
drone has 8pc IP-Cameras Video + data Type with UDP protocol.
This information is all entered into one network switch.
If we want to get this information inside the Ground control station, đó là 150 km away, what would you suggest?
Drone Transmitter Side:
- Camera IP (2M pixel)
- Camera IP (2M pixel)
- Camera IP (2M pixel)
- Camera IP (2M pixel)
- Camera IP (2M pixel)
- Camera IP (2M pixel)
- Camera IP (2M pixel)
- Camera IP (2M pixel)
- UDP Data (10KB)
- UDP Data = 4Mbps
- Network switch
- Phạm vi: 100~150km
GCS Side: Trạm điều khiển mặt đất
- 2 Hdmi Monitor for Video
- 1 Computer For Data
- We want to connect to Aviation ip cameras.
- And also PING all aviation Ip address
Hiện nay, the one that can basically meet customer needs is Vcan1806-100Mbps-2x10WPA.
Table of Contents
FAQ
Q1: Whether a directional antenna is required for optimal signal reception. or omni antenna?
A1: It is better to use one fiberglass omnidirectional antenna and one ăng-ten định hướng phẳng.

1. Frequency Band Requirements
- băng tần L & S-band Support
- Dual-band operation is required, likely for satellite communications, rađa, or airborne datalinks.
- Clarify specific frequency ranges (e.g., băng tần L: 1–2 GHz, S-band: 2–4 GHz) and ensure coexistence mechanisms (e.g., filters/duplexers) to prevent inter-band interference.
2. Bộ khuếch đại công suất (PA) Specifications
- 2×20W RF Output
- Dual-channel architecture with independent 20W amplification per channel, enabling redundancy or simultaneous dual-band transmission.
- Critical considerations: Thermal management (for airborne environments), PA efficiency optimization (e.g., GaN technology), and EMI/EMC compliance.
3. Interface Configuration
- Giao diện mạng
- 2× RJ45 ports: Support 100 Mbps Ethernet throughput; verify protocol compatibility (e.g., TCP/IP, VLAN tagging if needed).
- Truyền thông nối tiếp
- 1× bidirectional RS232 port: Ensure full-duplex operation for control commands or low-rate data transmission.
4. Performance Metrics
- Tốc độ dữ liệu: 100 Mb/giây
- Requires high-efficiency modulation (e.g., 256-QAM, OFDM) and sufficient RF channel bandwidth.
- Max Range: 200 km
- Perform detailed link budget analysis: Account for Tx power (20ở PA), tăng ăng-ten, receiver sensitivity, free-space path loss, and atmospheric/terrain attenuation (critical for L/S-band over 200 km).
5. Airborne Design Constraints
- Environmental Compliance
- Meet DO-160 standards for vibration, sốc, nhiệt độ (-40°C đến +70°C), and EMI/EMC.
- Physical Integration
- Nhỏ gọn, lightweight design compliant with aviation form factors (e.g., ARINC 600). Prioritize heat dissipation and power efficiency.
6. Key Challenges & Open Questions
- Application Context
- Clarify use case (quân đội, commercial UAV, or manned aircraft). Are encryption or anti-jamming capabilities required?
- Certification
- Confirm regulatory needs: FAA/EASA certifications (e.g., DO-254/178C) or military standards (e.g., MIL-STD-810).
- Tích hợp
- Define interface compatibility (e.g., ARINC 429, MIL-STD-1553) with existing avionics systems.
- Antenna Design
- Specify antenna type (directional vs. đa hướng) and mounting constraints.
Technical Recommendations
- RF Link Optimization
- Use adaptive modulation (AMC) and forward error correction (FEC) to balance data rate and range.
- Quản lý nhiệt
- Implement GaN-based PAs for high efficiency and integrate active cooling (e.g., liquid cooling or forced airflow).
- Dự phòng & Độ tin cậy
- Design dual-channel redundancy for mission-critical airborne operations.
- nguyên mẫu & Kiểm tra
- Conduct field trials to validate 200 km range under real-world conditions (e.g., độ cao, sự can thiệp).
Bản tóm tắt
The customer requires a dual-band, high-power airborne communication system optimized for long-range (200 km), tốc độ cao (100 Mb/giây) truyền dữ liệu. Success hinges on balancing thermal performance, cân nặng, and RF efficiency while meeting stringent aviation standards. A phased approach—starting with detailed link budget modeling and prototype testing—is recommended to mitigate risks.

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