rincian produk

Rumah Produk

0.02°/h Bias Stability MEMS Gyroscope Chip for Inertial Measurement Unit

Nama merek:	Firepower
Nomor Model:	MGZ221HC
Moq:	1
harga:	Dapat dinegosiasikan
Ketentuan Pembayaran:	T/T
Kemampuan Penyediaan:	500/bulan

Informasi Rinci

Deskripsi produk

Informasi Rinci

Tempat asal:

CINA

Nama Produk:

PCB GYRO

Jangkauan:

400 derajat/dtk

Lebar pita:

>200Hz

Resolusi:

24 bit

Faktor skala:

16000 lb/derajat/dtk

Penundaan (disesuaikan):

<1,5 md

Ketidakstabilan Bias:

0,5 derajat/jam

Kemasan rincian:

spons + kotak

Menyediakan kemampuan:

500/bulan

Menyoroti:

0.02°/h MEMS gyroscope chip

MEMS gyroscope for inertial measurement

high stability fiber optic gyro

Deskripsi produk

0.02°/h Bias Stability MEMS Gyroscope Chip for Inertial Measurement Unit

Our MEMS gyroscope chip delivers high-precision angular rate sensing for advanced inertial navigation and motion control applications. Designed with aerospace-level reliability and industrial-grade durability, it provides ultra-low noise, low bias instability, and excellent temperature stability for platforms that require long-term accuracy and robust performance.

Engineered for UAVs, autonomous robots, and industrial equipment, this MEMS gyro chip offers fast dynamic response, compact form factor, and low power consumption — making it ideal for embedded navigation systems and precision motion platforms.

PCB Design Guidelines

Decoupling capacitors for pins VCP, VREF, VBUF, and VREG should be placed as close to the pins as possible with minimized trace resistance
Other ends of decoupling capacitors for VREF, VBUF, and VREG should connect to nearest AVSS_LN and then to signal ground via a magnetic bead
Decoupling capacitors for VCC and VIO must be placed close to corresponding pins
VCC operation requires about 35mA current - use wide PCB traces for voltage stability
Avoid routing under the package for smooth assembly
Position components away from stress concentration areas, heat sources, and mechanical contact points

Technical Specifications

Performance	Unit	MGZ332HC-P1	MGZ332HC-P5	MGZ318HC-A1	MGZ221HC-A4	MGZ330HC-O1	MGZ330HC-A1
Range	deg/s	400	400	400	400	400	100
Band Width @3DB customized	Hz	90	180	200	200	300	50
Output accuracy(digital SPI)	bits	24	24	24	24	24	24
Output rate(ODR)(customized)	Hz	12K	12K	12K	12K	12K	12K
Delay(customized)	ms	<3	<1.5	<1.5	<1.5	<1	<6
Bias stability	deg/hr(1o)	<0.05	<0.05	<0.1	<0.5	<0.1	<0.02
Bias stability (1σ 10s)	deg/hr(1o)	<0.5	<0.5	<1	<5	<1	<0.1
Bias stability (1σ 1s)	deg/hr(1o)	<1.5	<1.5	<3	<15	<3	<0.3
Bias error over temperature (1σ)	deg/hr(1o)	<5	<5	<10	<30	10	5
Bias temperature variations, calibrated(1σ)	deg/hr(1o)	<0.5	<0.5	<1	<10	<1	<0.5
Bias repeatability	deg/hr(1o)	<0.5	<0.5	<0.5	<3	<0.3	<0.1
Scale factor at 25°C	lsb/deg/s	20000	20000	16000	16000	20000	80000
Scale factor repeatability (1σ)	ppm(1o)	<20ppm	<20ppm	<20ppm	<20ppm	<100ppm	<100ppm
Scale factor vs temperature (1σ)	ppm(1o)	100ppm	100ppm	<100ppm	<100ppm	<300ppm	<300ppm
Scale factor non-linearity (1σ)	ppm	100ppm	100ppm	<150ppm	<150ppm	<300ppm	<300ppm
Angular random walk(ARW)	°/√h	<0.025	<0.025	<0.05	<0.25	<0.05	<0.005
Noise(Peak to Peak)	deg/s	<0.15	<0.3	<0.35	<0.4	<0.25	<0.015
GValue sensitivity	°/hr/g	<1	<1	<1	<3	<1	<1
Vibration rectification error(12gRMS,20-2000)	°/hr/g(rms)	<1	<1	<1	<3	<1	<1
Power-on time (valid data)	s	750m
Sensor Resonant Frequency	hz	10.5k-13.5K

Environmental Specifications

Impact (power on): 500g, 1ms
Impact resistance (power off): 10000g, 10ms
Vibration(power on): 18g rms (20Hz to 2kHz)
Working temperature: -40℃ to +85℃
Store temperature: -55℃ to +125℃
Supply voltage: 5±0.25V
Current consumption: 45ma

Installation Guidelines

High-performance MEMS gyroscope is a high-precision test equipment. To achieve optimal design performance, consider these installation recommendations:

Evaluate sensor placement using thermal analysis, mechanical stress simulation (bending measurement/FEA), and impact robustness testing
Maintain appropriate distance from:
- PCB thickness recommendations: 1.6-2.0mm to minimize inherent stress
- Buttons/mechanical stress points
- Heat sources (controllers, graphics chips) that may raise PCB temperature
Avoid placement in areas prone to mechanical stress, warping, or thermal expansion

Tag:

Sensor Akselerometer Gyro

IMU Accelerometer Gyro

Akselerometer lentur kuarsa

gyro serat optik

Sistem Navigasi Inersia

Penemu Utara Gyro

Sensor Magnetometer

Sensor Akselerometer Gyro

IMU Accelerometer Gyro

Akselerometer lentur kuarsa

gyro serat optik

Sistem Navigasi Inersia

Penemu Utara Gyro

Sensor Magnetometer

rincian produk

0.02°/h Bias Stability MEMS Gyroscope Chip for Inertial Measurement Unit

0.02°/h Bias Stability MEMS Gyroscope Chip for Inertial Measurement Unit

0.02°/h MEMS gyroscope chip

MEMS gyroscope for inertial measurement

high stability fiber optic gyro

Gyro Serat Optik Sumbu Tunggal

Gyro Presisi Tinggi 250hz

Meter Inersia Sudut Bias Rendah

Sensor optik giroskopis serat optik presisi tinggi tingkat kebisingan rendah biaya yang wajar

Giroskop Serat Optik 50mm x 50mm x 32mm dengan Rentang ±500°/s

Sensor Giroskop Serat Optik Terpadu Fotonic Silikon Pengganti Fizoptika Vg1703

Mini Rs422 Fiber Gyro Baik Non Linearitas Zero Bias Stabilitas

Tidak ada waktu pemanasan Giroskop serat optik dengan rentang dinamis luas 200g Output Mode RS-422