| 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)σ） |
| Recapture time | ≤ 2S (lock loss time not more than 30s) | |
| Measurement accuracy | Single point accuracy | Horizontal 4m (1)σ），Vertical 6m (1)σ），Speed accuracy 0.1m/s (1)σ） |
| Differential accuracy | Horizontal 1m (1)σ），Vertical 1m (1)σ），Speed accuracy 0.05m/s (1)σ） | |
| Data output frequency | Second pulse: frequency | 1Hz；Accuracy: 20ns (1)σ）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 |
| PPS second pulse interface | 1 A PPS second pulse output interface outputs RS422 PPS information | |
| 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 | |
