Products

GSXV7021 brings gyro capability to chip-scale integration. The 8.9×8.9×2.7mm package consumes as little as 4mW (0.9mA) with SPI/I2C dual interface and 16/24-bit angular rate output. Bias temperature drift only 0.0016°/s/°C with angular random walk 0.065°/√h. Built-in programmable digital filters and temperature sensor. From wearables and medical motion detection to industrial image stabilization—chip-level gyro sensing empowers everything.

GSGYR311F packs triaxial FOG performance into a 52×51×52mm cube weighing just 300g—one of the lightest in its class. Bias

GSGYR304F-H adopts a split architecture with separate sensing head and electronics. Bias stability

GSGYR301F features a slim Φ59×18.3mm circular package weighing

GSRBA500D is a solid-state digital-output accelerometer built on quartz flexible technology. Unlike traditional analog sensors, it delivers direct digital readings with fast start-up and minimal power draw. ±70g range and 22×22×14mm compact housing. Bias stability ≤100μg, second-order nonlinearity ≤80μg/g2, noise floor ≤10μg — delivering precision previously found only in larger devices. 400Hz bandwidth and 200g shock tolerance with -45°C to +85°C operation. Quartz design inherently resists shock and vibration, offering long-term stability analog accelerometers cannot match. The sensor consumes just 5mA at 15V, making it ideal for aerospace, aviation, navigation, military weapons, and vehicle systems where reliability and accuracy are mission-critical.

GSQAT160 holds the benchmark for high-temperature quartz accelerometers with continuous operation at 160°C (185°C optional). ±20g range in a 25.4×25.4×18.6mm flange-mount package weighing 55g. Resolution

GSQAMini125 packs quartz flex accelerometer performance into an extreme miniaturized φ18.8×21mm, 25g package. Withstands -45°C to +125°C (185°C optional) for high-temperature environments. ±20g range, bias stability ≤100μg, current output, and 1000g shock tolerance. This sensor is engineered specifically for MWD (measurement-while-drilling), geophysical exploration, and other confined high-temperature spaces where conventional sensors cannot survive.

GSACC303M delivers RS422 digital output with ±10g range (±100g optional) and 0.001g resolution. Nonlinearity ≤0.2%FS with built-in nonlinearity and cross-coupling correction ensures data integrity. Bias temperature drift only 0.01g maintains stability across temperature variations. The 55×55×35mm metal housing provides robust protection. Designed for inertial navigation systems and flight control where long-term precision and high resolution are non-negotiable.

GSACC302M provides RS422 digital output at 200Hz data rate from a 10~30VDC supply. Standard ±2g range with optional ±70g extends application flexibility. Resolution 0.002g with full temperature compensation and nonlinearity correction. The 55×55×35mm rugged housing withstands 4000g shock and is purpose-built for oil drilling, seismic monitoring, and other harsh industrial environments where plug-and-play reliability matters.

GSACC301M synchronizes three-axis acceleration sensing with ±3g range and 300mV/g analog output (0~3V). Resolution 0.001g and bandwidth ≥500Hz capture high-frequency dynamics, while

GSINS032C sets the benchmark with gyro bias ≤0.005°/h, pure inertial positioning

GSINS030C combines triaxial integrated FOG with quartz accelerometers in a 160×132×117mm, 3kg design. Gyro bias ≤0.01°/h delivers attitude

GSIMU010M packs precision-calibrated 3-axis gyro and accelerometer into a 22.4×22.4×9mm housing weighing under 10 grams. Gyro bias instability 2°/h and accelerometer bias 20μg deliver industrial-grade performance. Optional 1000Hz output supports high-dynamic applications. Aluminum alloy housing ensures durability across -40°C to +85°C environments. It has become the core sensing unit for UAVs, AGVs, smart agricultural machinery, and ROV dynamic control systems.

GSIMU005M features dual redundant gyro and accelerometer pairs within a 27×27×10mm compact footprint. This hardware-level backup architecture ensures continuous operation in mission-critical applications. Gyro bias

GSIMU001M offers a cost-effective path to high-performance inertial measurement without compromising reliability. Sealed housing protects internal sensors in industrial environments. RS-422 digital output delivers 200Hz update rates with gyro range ±200°/s and 8000g shock tolerance. Available in Φ39.5mm cylindrical or 26.5mm square enclosures to fit diverse mechanical layouts. Ideal for automotive electronics, antenna stabilization, and aircraft attitude reference systems.

GSQRS14-102 features a monolithic quartz sensing element for solid-state reliability. Bias ≤0.05°/s (100s smoothing) with noise ≤0.004°/s and scale nonlinearity ≤0.05%. The 59.44×25.65×25.65mm, ≤50g package outputs analog voltage (0.5~4.5V) with built-in voltage regulation. 9~18V supply and 2-second startup. Designed for gimbal stabilization, camera anti-shake, and industrial fan control applications requiring robust angular rate sensing.

GSGYR323M approaches FOG-level precision with MEMS technology: bias ≤0.2°/h, scale nonlinearity ≤0.02%, resolution ≤0.01°/s. The ±500°/s range and

GSGYR131M utilizes a quartz crystal resonant element for reliable single-axis rate sensing. Bias stability ≤15°/h within ±75°/s range. The 35×35×40mm,

GSGYR201F provides dual-axis synchronized angular rate sensing in a 64×60×40mm integrated package weighing 170~200g. Standard grade bias

GSGYR112F offers four accuracy grades from Standard to HH, with highest bias

GSACC202M offers a lightweight dual-axis solution at just 20g. ±2g range with 1000mV/g sensitivity and analog output deliver 0.001g resolution. Bandwidth ≥50Hz (400Hz optional) supports various dynamic measurements. Operating from -40°C to +70°C with 2000g shock survival, this 18.8×12.7×8.4mm sensor is the top choice for flight control and seismic vibration monitoring requiring two-axis sensing.

GSGYR101F is a digital closed-loop FOG delivering bias

GSACC131Q eliminates I/F conversion with TTL direct digital readout at 1kHz output rate. Available in L, Standard, and H accuracy grades, with highest bias stability ≤20μg (1 month) and scale factor 1,000,000 LSB/g. The φ25.4×30mm package comes in two housing options (A/B). This digital quartz accelerometer simplifies system integration across inertial navigation, flight control, and measurement systems without compromising precision.

GSACC111Q achieves μg-level precision with bias stability ≤10μg, scale factor temp sensitivity 10ppm/°C, and 2nd-order nonlinearity ≤10μg/g2. The φ25.4×29mm, 75g package delivers current output with user-selectable sampling resistors. Operating from -45°C to +80°C, this premium accelerometer serves satellite microgravity measurement, inertial navigation, and flight control applications demanding the highest levels of accuracy.

GSACC101M delivers high-sensitivity single-axis vibration sensing with ±1g range and 1000mV/g analog output. Resolution better than 0.001g and nonlinearity ≤0.5%FS ensure accurate low-frequency acceleration measurement. The 19.5×18.8×8.4mm package draws just 2mA from a 5V supply with full temperature compensation. Designed for flight control stabilization and seismic detection where precision at low frequencies is critical.

GSINS025C achieves attitude

GSINS016C integrates high-performance FOG and quartz accelerometers within a 110×110×100mm, 1.6kg compact chassis. Heading alignment accuracy better than 0.1° (1σ) with pure inertial navigation better than 2nm/h (CEP). Supports GNSS, DVL, and odometer data fusion for enhanced positioning resilience. Built for naval, land, aviation, and defense applications where size and weight matter without sacrificing accuracy.

GSTIM300 delivers 0.5°/h gyro bias stability in a MEMS design that meets general military standards. RS-422 interface supports 500Hz high-speed data output, while 5000g shock tolerance and -45°C to +85°C operation ensure survival in extreme environments. Integrated attitude solving (pitch/roll) reduces external processing needs. M4 screw mounting provides secure mechanical integration for guided weaponry, aviation stabilization, and dynamic measurement tasks.

GS16488 combines 3-axis gyro, accelerometer, magnetometer, and barometer into a true 10-DOF inertial solution. With gyro bias 0.5°/h and accelerometer bias 10μg, it delivers precision previously found only in larger systems. The 44×47×14mm package supports SPI interface and operates from -40°C to +85°C. Designed as a drop-in replacement for imported IMUs, it serves gimbal stabilization, rail inspection, and UAV navigation with uncompromised performance.

GSMTI3 is a self-contained Attitude Heading and Reference System (AHRS). This fully functional self-contained module can be easily designed by adding limited hardware components.