Fiber Optic Gyroscope Imu

US$7,746.00 / Piece

Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation pictures & photos

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What is Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation

Name: Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation
Uploaded: 2025-12-21T08:53:09+08:00
Description: Specification Parameters Unit Requirement Gyroscope Zero bias stability (1σ) °/h ≤0.2 Zero bias repeatability (1σ) °/h ≤0.2 Random walk coefficient °/ h1/2 ≤0.04 Scale factor nonlinearity ppm ≤100 Sca

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About this Item

Price

Min. Order Reference FOB Price

1 Piece US$7,746.00 / Piece

Sepcifications

Type Sensor
Output Signal Type Digital Output
Measuring Shaft Quantities Three
IP Rating IP67
Certification CE
Transport Package Box and Sponge
Specification 33*27*8mm
Trademark ML
Origin China
Brand Micro Magic

Product Description

Specification Parameters Unit Requirement Gyroscope Zero bias stability (1σ) °/h ≤0.2 Zero bias repeatability (1σ) °/h ≤0.2 Random walk coefficient °/ h1/2 ≤0.04 Scale factor nonlinearity ppm ≤100 Scale factor asymmetry ppm ≤100 Scale factor repeatability ppm ≤50 Measuring range °/s -300~+300 ...

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Hangzhou Maixinminwei Technology Co., Ltd.

Diamond Member Since 2024

Audited Supplier

Main Products Fog, Mems Imu, Inclinometer, Quartz Accelerometer, Mems Accelerometer, Mems Gyroscope, Fog ...
Address Room 215, 2nd Floor, Building 7, No. 1180, Bin'an Road, Changhe Sub-district, Binjiang District, Hangzhou City, Zhejiang Province
Main Markets Southeast Asia, Mid East, Western Europe
Average Lead Time Peak Season Lead Time: within 15 workdays
Off Season Lead Time: within 15 workdays

Fiber Optic Gyroscope Imu Comparison

	Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation Contact Now	Quick View Precision Fiber Optic Inertial Navigation for Enhancing Navigation Solutions Contact Now	Quick View Solid-State Fiber Optic Gyroscope for Navigation and Attitude Sensing Contact Now	Quick View Precision Inertial Navigation System for Uavs and Rotorcraft Contact Now	Quick View Fully Autonomous Fiber Optic Navigation System for Robots and Drones Contact Now

Transaction Info
	Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation Contact Now	Quick View Precision Fiber Optic Inertial Navigation for Enhancing Navigation Solutions Contact Now	Quick View Solid-State Fiber Optic Gyroscope for Navigation and Attitude Sensing Contact Now	Quick View Precision Inertial Navigation System for Uavs and Rotorcraft Contact Now	Quick View Fully Autonomous Fiber Optic Navigation System for Robots and Drones Contact Now
Price	US$7,746.00 / Piece	US$33,100.00 / Piece	US$9,720.00 / Piece	US$139,400.00 / Piece	US$33,100.00 / Piece
Min Order	1 Piece	1 Piece	1 Piece	1 Piece	1 Piece
Payment Terms	-	-	-	-	-
Quality Control
Product Certification	CE	ISO	ISO	ISO	ISO
Management System Certification	-	-	-	-	-
Trade Capacity
Export Markets	Southeast Asia, Mid East, Western Europe	North America, South America, Eastern Europe, Southeast Asia, Mid East, Eastern Asia, Western Europe	North America, South America, Eastern Europe, Southeast Asia, Mid East, Eastern Asia, Western Europe	North America, South America, Eastern Europe, Southeast Asia, Mid East, Eastern Asia, Western Europe	North America, South America, Eastern Europe, Southeast Asia, Mid East, Eastern Asia, Western Europe
Annual Export Revenue	-	-	-	-	-
Business Model	-	-	-	-	-
Average Lead Time	Peak Season Lead Time: within 15 workdays Off Season Lead Time: within 15 workdays	Peak Season Lead Time: 3-6 months Off Season Lead Time: 1-3 months	Peak Season Lead Time: 3-6 months Off Season Lead Time: 1-3 months	Peak Season Lead Time: 3-6 months Off Season Lead Time: 1-3 months	Peak Season Lead Time: 3-6 months Off Season Lead Time: 1-3 months
Product Attributes
Specification	Type: Sensor; Output Signal Type: Digital Output; Measuring Shaft Quantities: Three; IP Rating: IP67; Brand: Micro Magic;	Type: Universal Optical Gyro Attitude Reference Series; Output Signal Type: Digital Output; Measuring Shaft Quantities: Three; Accuracy Grade: ≤0.04°/H; IP Rating: IP6X; Customized: Customized; Bias Repeatability: ≤0.01°/Hr,1σ; Scale Factor Accuracy: ≤20ppm; Random Walk: ≤0.003°/√Hr; Angular Rate: ≥±400°/Sec; Angular Acceleration: >25g; Startup Time: ≤10sec; Input/Output: 3 RS422 Full-Duplex Serial Ports, 1 100m Ethernet; Pure Inertia: ≤0.04°/H; Power Consumption: <15W; Dimensions(mm×Wmm×Hmm): 130×130×110; Temperature: -40℃~60℃; Shock: 15g,Half-Sine Wave 11ms; Input Voltage: DC24V(±25%); Vibration: 20~2000Hz,6.06g;	Type: Navigation-Grade Fiber Optic Gyroscope Series; Output Signal Type: Digital Output; Measuring Shaft Quantities: Three; Accuracy Grade: 0.1°/H~0.04°/H; IP Rating: IP6X; Customized: Customized; Dynamic Range: ≥±400°/S; Bias in-Run: <1°/H; Accuracy: 0.1°/H~0.04°/H; Angular Random Walk: <0.03°/√Hr,1σ; Vibration Screening: 20~2000Hz,6.06g; Bandwidth: >200Hz; Turn on Time: 10s; Output Signal Format: RS-422; Output Signal Update Rate: 500Hz~4000Hz; Operating Temperature: - 40℃ ~ + 70℃; Storage Temperature: - 55℃ ~ + 85℃; Power Supply: 5V; Connector: J30jz/Xn9tjcal01; Power Consumption: ≤4.5W; Dimensions: 60×60×28;	Type: Aircraft Inertial Navigation System/Inertial Refer; Output Signal Type: Digital Output; Measuring Shaft Quantities: Three; Accuracy Grade: ≤1nm/6h; IP Rating: IP6X; Customized: Customized; Bias Repeatability: ≤0.008°/Hr; Scale Factor Accuracy: ≤5ppm; Random Walk: ≤0.003°/√Hr; Position Accuracy: ≤1nm/6h; Angular Rate: ≥±400°/Sec; Speed Accuracy: ≤0.2m/S; Alignment Time: ≤8min; Input/Output: 3 RS422 Full-Duplex Serial Ports, 1 100m Ethernet; Power Consumption: <40W; Dimensions(mm): 193×169×160; Temperature: -40℃~60℃; Shock: 15g,Half-Sine Wave 11ms; Input Voltage: DC24V(±25%); Cooling: Conduction to Mounting Plate; Vibration: 20~2000Hz,6.06g;	Type: Universal Optical Gyro Attitude Reference Series; Output Signal Type: Digital Output; Measuring Shaft Quantities: Three; Accuracy Grade: ≤0.05°/H; IP Rating: IP6X; Customized: Customized; Bias Repeatability: ≤0.03°/Hr,1σ; Scale Factor Accuracy: ≤20ppm; Random Walk: ≤0.005°/√Hr; Angular Rate: ≥±400°/Sec; Angular Acceleration: >25g; Startup Time: ≤10sec; Input/Output: 3 RS422 Full-Duplex Serial Ports, 1 100m Ethernet; Pure Inertia: ≤0.05°/H; Power Consumption: <15W; Dimensions(mm×Wmm×Hmm): 120×110×80; Temperature: -40℃~60℃; Shock: 15g,Half-Sine Wave 11ms; Input Voltage: DC24V(±25%); Vibration: 20~2000Hz,6.06g;
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