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UAV Satellite Navigation Receiver

SKU: MD-P00480·Spare Parts & Components·受注生産

UAV Satellite Navigation Receiver
UAV Satellite Navigation Receiver

概要

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.

技術仕様

Specifications. 主な仕様: 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。

技術仕様 — 1 groups
主な仕様: 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。

技術仕様

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

対応機体

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