What is Manned Aircraft Imu Module

Name: Manned Aircraft Imu Module
Uploaded: 2024-03-29T10:34:10+08:00
Description: IMU488M Hight Performance Inertial Navigation System (IMU) Inertial Measurement Unit Inertial Sensor Main Features - Precision 10 DoF MEMS Inertial Measurement Unit - Dynamic Range: Gyro ±45

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Price

Min. Order Reference FOB Price

1 Piece Negotiable

Sepcifications

Type Inertial Measurement Unit
Output Signal Type Digital Output
Measuring Shaft Quantities 10
Accuracy Grade 1degree/H
IP Rating IP67
Certification ISO
Customized Non-Customized
Transport Package Carton
Specification 47*44*14mm
Trademark SkyMEMS
Origin China
Dynamic Range Gyro: +-450deg/S, Acc: +-16g
Bias Stability Gyro: 1deg/H, Acc 30ug (Allan)
Working Temperature -40~+85degc
Interface Uart, Spi

Product Description

IMU488M Hight Performance Inertial Navigation System (IMU) Inertial Measurement Unit Inertial Sensor Main Features - Precision 10 DoF MEMS Inertial Measurement Unit - Dynamic Range: Gyro ±450°/s, Acc ±16g - Bias Stability: Gyro: 1°/h, Acc 30μg (Allan) - Full ...

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Nanjing Sky Mems Technology Co., Ltd.

Gold Member Since 2022

Audited Supplier

Business Type Manufacturer/Factory
Main Products Inertial Measurement Unit, Mems Accelerometer, Electronic Compass, Inclinometer, Fiber Optic Gyro, Gnss Ins Integrated Navigation System, Tilt Sensor, Imu
Registered Capital 1000000 RMB
Plant Area >2000 square meters
Management System Certification ISO 9001
Average Lead Time Peak Season Lead Time: one month
Off Season Lead Time: within 15 workdays

Inertial Measurement Unit Comparison

	Quick View Manned Aircraft Imu Module Contact Now	High Stability Quartz Accelerometer Single Axis Quartz Vibration Sensor Contact Now	Inertial Navigation Sensors for Reliable and Accurate Positioning Contact Now	Advanced Inertial Navigation System Equipped with Intelligent Algorithms and Advanced Features for Precise Navigation in Any Environment. Contact Now	Advanced Inertial Navigation Sensors Offering Unparalleled Accuracy and Reliability in Harsh Environment Contact Now

Transaction Info
	Quick View Manned Aircraft Imu Module Contact Now	High Stability Quartz Accelerometer Single Axis Quartz Vibration Sensor Contact Now	Inertial Navigation Sensors for Reliable and Accurate Positioning Contact Now	Advanced Inertial Navigation System Equipped with Intelligent Algorithms and Advanced Features for Precise Navigation in Any Environment. Contact Now	Advanced Inertial Navigation Sensors Offering Unparalleled Accuracy and Reliability in Harsh Environment Contact Now
Price	Negotiable	US $ 1,100.00-1,200.00/ pcs	US $ 2,500.00-4,000.00/ Piece	US $ 2,500.00-4,000.00/ Piece	US $ 2,500.00-4,000.00/ Piece
Min Order	1 Pieces	1 pcs	1 Pieces	1 Pieces	1 Pieces
Trade Terms	-	-	-	-	-
Payment Terms	T/T, Western Union, Money Gram	L/C, T/T	L/C, T/T	L/C, T/T	L/C, T/T
Quality Control
Product Certification	ISO	CE	CE	CE	CE
Management System Certification	ISO 9001	ISO 9001	ISO 9001	ISO 9001	ISO 9001
Trade Capacity
Export Markets	North America, South America, Eastern Europe, Southeast Asia, Africa, Oceania, Mid East, Eastern Asia, Western Europe	Eastern Europe, Southeast Asia, Mid East	Eastern Europe, Southeast Asia, Mid East	Eastern Europe, Southeast Asia, Mid East	Eastern Europe, Southeast Asia, Mid East
Annual Export Revenue	-	-	-	-	-
Business Model	OEM, ODM, Own Brand	OEM, ODM, Own Brand	OEM, ODM, Own Brand	OEM, ODM, Own Brand	OEM, ODM, Own Brand
Average Lead Time	Off-season: within 15 Day(s) Peak-season: 1 Month(s)	Off-season: within 15 Day(s) Peak-season: within 15 Day(s)	Off-season: within 15 Day(s) Peak-season: within 15 Day(s)	Off-season: within 15 Day(s) Peak-season: within 15 Day(s)	Off-season: within 15 Day(s) Peak-season: within 15 Day(s)
Product Attributes
Specification	Type: Inertial Measurement Unit; Output Signal Type: Digital Output; Measuring Shaft Quantities: 10; Accuracy Grade: 1degree/H; IP Rating: IP67; Customized: Non-Customized; Dynamic Range: Gyro: +-450deg/S, Acc: +-16g; Bias Stability: Gyro: 1deg/H, Acc 30ug (Allan); Working Temperature: -40~+85degc; Interface: Uart, Spi;	Type: Quartz Flexure Accelerometer; Output Signal Type: Analog Output; Measuring Shaft Quantities: Single; Accuracy Grade: 3mg; IP Rating: IP67; Customized: Customized; Function: Vibration Test; Operating Voltage: 12~18 VDC; Insulation Resistance: 50ohm, @50VDC; Power Consumption: <480MW, @15VDC; Current Consumption: <16mA, @15VDC; Weight: 80g; Measuring Range: 50g; Threshold Value: 5ug; Scale Factor K1: 1.3+/-0.2 Ma/G;	Type: Inertial Navigation; Output Signal Type: Digital Output; Measuring Shaft Quantities: Three; Accuracy Grade: 2cm; IP Rating: IP67; Customized: Customized; Positionin G Accuracy: 2cm+1ppm Gnss Valid Rtk; Heading Accuracy: 0.1deg; Attitude Accuracy: 0.02deg (RMS); Power Source: 9-36V; Weight: <1kg;	Type: Inertial Navigation; Output Signal Type: Digital Output; Measuring Shaft Quantities: Three; Accuracy Grade: 2cm; IP Rating: IP67; Customized: Customized; Positionin G Accuracy: 2cm+1ppm Gnss Valid Rtk; Heading Accuracy: 0.1deg; Attitude Accuracy: 0.02deg (RMS); Power Source: 9-36V; Weight: <1kg;	Type: Inertial Navigation; Output Signal Type: Digital Output; Measuring Shaft Quantities: Three; Accuracy Grade: 2cm; IP Rating: IP67; Customized: Customized; Positionin G Accuracy: 2cm+1ppm Gnss Valid Rtk; Heading Accuracy: 0.1deg; Attitude Accuracy: 0.02deg (RMS); Power Source: 9-36V; Weight: <1kg;
Supplier Name	Nanjing Sky Mems Technology Co., Ltd.	Shenzhen Avionics Technology Co., Limited	Shenzhen Avionics Technology Co., Limited	Shenzhen Avionics Technology Co., Limited	Shenzhen Avionics Technology Co., Limited
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