Beijing Oriental Liaoning Technology Co., Ltd. (Beijing Oriental Liaoning Technology Co., Ltd.)
Kuæa>Proizvodi>PNS100-BGI BDS/GPS/MEMs Precision Combined Navigation System
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PNS100-BGI BDS/GPS/MEMs Precision Combined Navigation System
PNS100-BGI BDS/GPS/MEMs Precision Combined Navigation System
Detalji proizvoda

PNS100-BGI BeiDou/GPS/MEMs Precision Combined Navigation System ee inertial measurement unit ye tɔ̈u në MEM technology ku ye tɔ̈u në Beidou multi-mode satellite navigation chipOTrack-32 BeiDou/GPS/GLONASS(Technology of Satellite Navigation Receiver Units for Integrated Design and Developed Small Inertiality) (Technology of Satellite Navigation Receiver Units for Integrated Design and Developed Small Inertiality) (Technology of Satellite Navigation Receiver Units for Integrated Design and Developed Small Inertiality)/Satelit Combined Navigator (Satelit Combined Navigator) A baara ye kɔrɔ, a tɛ̈n ye kɔrɔ, a tɛ̈n ye kɔrɔ, a tɛ̈n ye kɔrɔ, a tɛ̈n ye kɔrɔ, a tɛ̈n ye kɔrɔ.

A lëu bï ya tɛ̈n yenë kɔc cɔl a ye kɔc cɔl a ye kɔc cɔl a ye kɔc cɔl a ye kɔc cɔl a ye kɔc cɔl a ye kɔc cɔl a ye kɔc cɔl a ye kɔc cɔl a ye kɔc cɔl
Ku dɛ̈t peei, navigateur kënë alëu bï wël cïmën de geomagnetic, temperature, ku air pressure ya yök në kë wïc raan ye luɔɔi.

Teknoloji
1Integrated deep coupling--Adopting MatureMEMSInertial Devices and Beidou Multimode Satellite Navigation Chips (Inertial Devices and Beidou Multimode Satellite Navigation Chips)OTrack-32 BeiDou/GPS/GLONASS), Integrated Integrated Deep Coupling Design, Not Only ImprovedPNS100A ye tɛmɛ, a ye tɛmɛ, a ye tɛmɛ, a ye tɛmɛ, a ye tɛmɛ, a ye tɛmɛ, a ye tɛmɛ, a ye tɛmɛ, a ye tɛmɛ, a ye tɛmɛ, a ye tɛmɛPNS100A koom koom koom koom koom koom koom koom koom koom koom koom koom koom koom koom koom koom koom koom koom koom koom koom koom koom koom koom koom koom koom koom koom330 K.
2Offline kalibrasiɔn--Ka tɛmɛ tekinoloji ye cɔl carrier motion state recognition, gravity field, Kalman filter zero speed constraint, ka tɛmɛ gyroscope ku accelerometer ye cɔl electric zero real time online calibration.
3ka tɔt4 Satelit bɛ se ka baara cok--False distance yök në inertial unit ku satellite navigation chip në processor tök/False distance measurement value (Kä ye kek tɛ̈n ye kek tɛ̈n ye kek tɛ̈n ye kek tɛ̈n ye kek tɛ̈n ye)
4Monitoring Integrity--Lɔ̈ɔ̈m de teknoloji ye kek tɛ̈n yenë kek tɛ̈n yenë kek tɛ̈n yenë kek tɛ̈n yenë kek tɛ̈n yenë kek tɛ̈n yenë kek tɛ̈n yenë kek tɛ̈n yenë kek tɛ̈n yen
5Kɔl-kɔl-kɔl-kɔl-kɔl-kɔl-kɔl-kɔl-kɔl-kɔl-kɔl-kɔl-kɔl-kɔl--Magnetic sensors, global magnetic bias database, and rapid search and calibration technology, magnetic field stability conditions, can achieve rapid magnetic sensors helping north. Magnetic sensors, global magnetic bias database, and rapid search and calibration technology, magnetic field stability conditions, can achieve rapid magnetic sensors helping north. Magnetic sensors, global magnetic bias database, and rapid search and calibration technology,
6Hardware Synchronization--Satelit Navigation InsidePPSSecond pulse signals ye hardware synchronization looi, ka tɛmɛ tɛmɛ tɛmɛ tɛmɛ tɛmɛ tɛmɛ tɛmɛ tɛmɛ tɛmɛ tɛmɛ tɛmɛ tɛmɛ tɛmɛ tɛmɛ tɛmɛ tɛ

PNS100 Kuɔɔny

Tɛmnɛ tɛmnɛ tɛmnɛ tɛmnɛ tɛmnɛ tɛmnɛ tɛmnɛ tɛmnɛ tɛmnɛ tɛmnɛ tɛmnɛ
(1σ)
Horizontal Position Precision
5.0mSatellite signal interruption time is not greater than a satellite signal interruption time is not greater than a satellite signal interruption time is not greater than a satellite signal interruption time is not greater than a satellite signal interruption time is not greater than a satellite signal interruption time10s
80m(Satellite signal interruption time is not greater than)2minStatistics of vehicle testing results, sample number is greater than20
Kɛnɛya kɛnɛya
(1σ)
Kɛnɛya tɛmɛ tɛmɛ tɛmɛ tɛmɛ tɛmɛ tɛmɛ tɛmɛ tɛmɛ tɛmɛ tɛmɛ
0.05m/s
Speed measurement accuracy
0.10m/s
Waktu tɛmɛ
1PPS
±100ns
Hakkil kɛ̈l
(1σ)
Tilt angle
0.3°(Satelit Signal valid) (Satelit Signal valid) (Satelit Signal valid)
Horizontal kuɛl
0.3°(Satelit Signal valid) (Satelit Signal valid) (Satelit Signal valid) (Satelit Signal valid) (Satelit Signal valid) (Satelit Signal valid) (Satelit Signal valid) (Satelit Signal valid) (Satelit Signal valid) (Satelit Signal valid) (Satelit Signal valid) (Satelit Signal valid)
Rotational angle
0.6°(Satelit Signal valid) (Satelit Signal valid) (Satelit Signal valid)
Waktu start
Satelit re-capture
<>
Satelit Hot Launch
1s
Satelit Cold Launch
35s
Kombinasyon Start
+30s(Kɔɔr ye rot looi ka dɔŋ1m/s
Data output
Data navigation
Binary formats (tɛ̈n, tɛ̈n, tɛ̈n, tɛ̈n)
Raw Data
Satellite raw channel data, inertial sensor raw data
Interface
Lɔ̈k / Lɔ̈k
RS232/RS422
Lɔ̈k update rate
50Hz
Bandwidth ye gam
100Hz
Data Interface
IP50-14
Antenna Connector
SMA
Lɔ̈k Voltage
9V~36VDC
Fiziki
Volume
106.5mm×83.5mm×57.5mm
Weight ye
340g
Power consumption
3W@24VDC
Temperature de luɔi
-40~ +85
Anti-impact
1000g10ms
Anti-Vibration
8g20 Hz~2000 Hz
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