RS422 IMU Sensor 500º/s Gyro Range 16g Accelerometer
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RS422 Output IMU Six Output Inertial Sensor Analog Of STIM300 Electrical interface The electrical connector of IMU300C-A0-IMU product is J30J-15 TJL, and the specific contact definition and allocation are shown in the following table: Stitch number Name ......
Shenzhen Fire Power Control Technology Co., LTD
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200Hz Single Axis Gyro Sensor with High Bias Stability and RS422 Output for Precision Measurement
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...Gyro Sensor , Gyroscope Sensor Module High Bias Stability Feature Whole temperature range compensation and Nonlinear correction High Bias stability Digital RS422 output Data Fusion and Noise compensation Application fields High-speed rotating smart shells Multiple remote extended-range rockets Technical Specifications Type K-ARS-1500A K-ARS-1500D Electric character Input voltage 6±0.1VDC Input current ≤150mA Output Mode RS422...
Xi'an Kacise Optronics Co.,Ltd.
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GY-521 MPU6050 3 Axis Analog Gyro Sensors Module 3-5V
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...gyro sensors+ 3 Axis Accelerometer Module printed circuit assembly Product parameters Chip: MPU-6050 Power supply: 3-5V(Internal low differentianl voltage stabilization) Communication mode: Standard IIC communication protocol Chip built-in: 16bit the AD converter,16-bit data output Gyroscope range: ±250 500......
Shenzhen Canyi Technology Co., Ltd.
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GY-521 MPU-6050 3 Axis Gyro Sensor , Gyroscope Sensor Module For Arduino 3-5V
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3-5V GY-521 MPU-6050 3 Axis Gyroscope Acceleration Sensor Module Specification Chip MPU-6050 Power supply 3-5V Gyroscope range +/-250 500 1000 2000°/s Acceleration range +/-2 +/-4 +/-8 +/-16g Communication standard IIC communication agreement Chip built......
Oky Newstar Technology Co., Ltd
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ODM Supported UNIVO UBFS-DY Navigation System with Gyro Sensors and RS422 Output Form
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Beijing Universe Technologies Co., Ltd.
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Aviation Navigation TDF41A Airborne Optical Gyro Inertial Navigation System with ≤500μg Bias Repeatability, ≤0.03°/√hr Random Walk, and ≤0.2° Pitch & Roll Accuracy
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Aviation Navigation TDF41A Airborne Optical Gyro-Inertial Navigation 1 Introduction The airborne optical gyro inertial navigation system (INS) utilizes optical gyros and quartz accelerometers as its core sensors, employing either a strapdown or dithered (......
QINGDAO NAVI OPTICS TECHNOLOGY CO.,LTD
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2Kg 2 Axis Electro Optic System Sensor Uncooled LWIR Resolution 640x512
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... EO sensor , resolution 640x512 uncooled LWIR and 4km laser rangefinder,360° continuous rotation servo motor, , the total weight about 2.4kg.......
Chengdu Honpho Technology Co., Ltd.
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Merak-50ST Three-Axis FOG Fiber Optic Gyro Navigation System RS422
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FOG(Merak-50ST) This FOG system utilizes a distributed 1(electronics)+3(sensors) configuration with all-digital closed-loop processing, specifically designed to minimize navigation system alignment time. Technical merits: 1) Adjustable performance ......
CSSC Star&Inertia Technology co.,ltd.
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High Precision Navigation Fog Gyro 12*12*3.9cm RS422 Single Axis Gyroscope For UAVs
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Essential details MOQ:1 Size:L(12)*W(12)*H(3.8) cm Specification Number:LKF-FS120H Product Introduction Introduction LKF-FS120H is an inertial angular rate sensor based on the optical Sagnac effect, which is used to measure the angular rate of the carrier......
Wuhan Liocrebif Technology Co., Ltd
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