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UAV Satellite Navigation Receiver

SKU: MD-P00480·Spare Parts & Components·Made to Order

UAV Satellite Navigation Receiver
UAV Satellite Navigation Receiver

Overview

Product introduction and use The UAV satellite navigation receiver is a wireless link between the airborne and the ground. The UAV-specific satellite navigation receiver.jpg makes a real-time difference between the mobile station and the base station, and accurately confirms the actual position of the UAV. Small size, beautiful appearance and high reliability, suitable for high-speed moving UAV systems and fields.

Technical specification

Specifications. Key specifications: Operating frequency point BDS B3 / 1268.52 MHz 10.23MHz, Anti-narrowband interference capability B3 frequency point anti-narrowband interference not less than 60dB, Dynamic measurement range Speed / 100m/s, Acceleration 1g, Positioning time Cold start time / 60s (C / a code, P code) (1) ), Recapture time 2S (lock loss time not more than 30s), Measurement accuracy Single point accuracy / Horizontal 4m (1) ),Vertical 6m (1) ),Speed accuracy 0.1m/s (1) ), Differential accuracy Horizontal 1m (1) ),Vertical 1m (1) ),Speed accuracy 0.05m/s (1) ), Data output frequency Second pulse: frequency / 1Hz ;Accuracy: 20ns (1) )The update rate of satellite navigation information is 10Hz, Airborne equipment Power supply interface / One power supply input interface: Input Voltage 5V 0.5V, PPS second pulse interface 1 A PPS second pulse output interface outputs RS422 PPS information, Receive differential information 1 Two receive ground differential information, two-way RS422, and the baud rate is 115200bps, Can bus interface A CAN bus interface with baud rate of 500kbps. The two-way can bus outputs satellite navigation information to the flight control computer, Ground equipment Power supply interface / One power supply input interface: input voltage 9v-32v, Send differential information 1 Send ground differential information, bidirectional RS232_A. The baud rate is 115200bps, Send reference information to ground computer 1 Send reference information, bidirectional RS232_B. The baud rate is 115bps, Second pulse frequency, 1Hz ;Accuracy 20ns (1) )The update rate of satellite navigation information is 10Hz, One power supply input interface Input Voltage 5V 0.5V.

Technical specification — 1 groups
Key specifications: Operating frequency point BDS B3 / 1268.52 MHz 10.23MHz, Anti-narrowband interference capability B3 frequency point anti-narrowband interference not less than 60dB, Dynamic measurement range Speed / 100m/s, Acceleration 1g, Positioning time Cold start time / 60s (C / a code, P code) (1) ), Recapture time 2S (lock loss time not more than 30s), Measurement accuracy Single point accuracy / Horizontal 4m (1) ),Vertical 6m (1) ),Speed accuracy 0.1m/s (1) ), Differential accuracy Horizontal 1m (1) ),Vertical 1m (1) ),Speed accuracy 0.05m/s (1) ), Data output frequency Second pulse: frequency / 1Hz ;Accuracy: 20ns (1) )The update rate of satellite navigation information is 10Hz, Airborne equipment Power supply interface / One power supply input interface: Input Voltage 5V 0.5V, PPS second pulse interface 1 A PPS second pulse output interface outputs RS422 PPS information, Receive differential information 1 Two receive ground differential information, two-way RS422, and the baud rate is 115200bps, Can bus interface A CAN bus interface with baud rate of 500kbps. The two-way can bus outputs satellite navigation information to the flight control computer, Ground equipment Power supply interface / One power supply input interface: input voltage 9v-32v, Send differential information 1 Send ground differential information, bidirectional RS232_A. The baud rate is 115200bps, Send reference information to ground computer 1 Send reference information, bidirectional RS232_B. The baud rate is 115bps, Second pulse frequency, 1Hz ;Accuracy 20ns (1) )The update rate of satellite navigation information is 10Hz, One power supply input interface Input Voltage 5V 0.5V.

Technical specifications

Specifications

Operating frequency point
BDS B3 / 1268.52 MHz 10.23MHz
Anti-narrowband interference capability
B3 frequency point anti-narrowband interference not less than 60dB
Dynamic measurement range
Speed / 100m/s
Acceleration
1g
Positioning time
Cold start time / 60s (C / a code, P code) (1) )
Recapture time
2S (lock loss time not more than 30s)
Measurement accuracy
Single point accuracy / Horizontal 4m (1) ),Vertical 6m (1) ),Speed accuracy 0.1m/s (1) )
Differential accuracy
Horizontal 1m (1) ),Vertical 1m (1) ),Speed accuracy 0.05m/s (1) )
Data output frequency
Second pulse: frequency / 1Hz ;Accuracy: 20ns (1) )The update rate of satellite navigation information is 10Hz
Airborne equipment
Power supply interface / One power supply input interface: Input Voltage 5V 0.5V
PPS second pulse interface
1 A PPS second pulse output interface outputs RS422 PPS information
Receive differential information
1 Two receive ground differential information, two-way RS422, and the baud rate is 115200bps
Can bus interface
A CAN bus interface with baud rate of 500kbps. The two-way can bus outputs satellite navigation information to the flight control computer
Ground equipment
Power supply interface / One power supply input interface: input voltage 9v-32v
Send differential information
1 Send ground differential information, bidirectional RS232_A. The baud rate is 115200bps
Send reference information to ground computer
1 Send reference information, bidirectional RS232_B. The baud rate is 115bps
Second pulse
frequency
1Hz ;Accuracy
20ns (1) )The update rate of satellite navigation information is 10Hz
One power supply input interface
Input Voltage 5V 0.5V

Compatible aircraft

This part fits the following platforms.

Fitment data pending — contact us with your aircraft model.

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