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Inertial Navigation System

Fiber Optic Inertial Measurement Unit , Closed Loop Fiber Optic Gyroscope

Name: Fiber Optic Inertial Measurement Unit , Closed Loop Fiber Optic Gyroscope
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: IMU300F
Price: 5,000.00 USD
Availability: InStock

Brand Name:	Firepower
Model Number:	IMU300F
MOQ:	1
Price:	negotiable
Payment Terms:	T/T
Supply Ability:	500/month

Detail Information

Product Description

Detail Information

Place of Origin:

CHINA

Certification:

CE ROHS

Product:

INS With GPS

Gyro Range:

±400°/s

Gyro Zero Bias Stability:

≤0.3°/h

Accelerometer Range:

±20g

Accelerometer Zero Bias Stability:

≤100µg

Voltage:

12-32V DC

Operating Temperature:

-40℃~+60℃

Packaging Details:

sponge+carton

Supply Ability:

500/month

Highlight:

Fiber Optic Inertial Measurement Unit

Closed Loop Fiber Optic Gyroscope

32V DC Fiber Optic Accelerometer

Product Description

The Fiber-Optic Inertial Measurement Unit Closed-Loop Fiber-Optic Gyroscope And An Accelerometer With High Performance

Overview

The fiber-optic inertial measurement unit IMU300F-DGI is composed of a three-axis closed-loop fiber-optic gyroscope and an accelerometer with high cost performance, and is realized through a multi-sensor fusion and navigation calculation algorithm to meet the requirements for accurate measurement of information such as attitude, course and position in application fields such as medium and high-precision mobile measurement systems and medium and large unmanned aerial vehicles.

Gyroscope	Measuring range	±400°/s / ±500°/s optional
Gyroscope	Zero bias stability	≤0.3°/h
Accelerometer	Measuring range	±20g
Accelerometer	Zero bias stability	≤100µg
Physical dimensions and electrical characteristics	Voltage	12-32V DC
	Power consumption	≤ 12W (steady state)
	Interface	2-channel RS232, 1-channel RS422, 1-channel PPS (LVTTL/422 level)
	Size	92.0 mm × 92.0 mm × 81.0mm (L, W, H)
	Weight	≤1.0kg
Environmental characteristics	Operating temperature	-40℃~+60℃
	Storage temperature	-45℃~+70℃
	Vibration	5 ~ 2000Hz, 6.06 G (with shock absorber)
	Impact	30g, 11 ms (with shock)
	Life span	> 15 years
	Continuous working time	>24h

Functions and indicators:

The system has inertial/satellite integrated navigation mode and pure inertial mode.

In the inertial/satellite integrated navigation mode, the satellite positioning information received by the internal GNSS receiver can be used for integrated navigation, and the pitch, roll, course, position, speed, time and other information of the carrier can be output; After the signal is lost, the position, velocity and attitude of the inertial solution are output, in which the pitch and roll are required to be kept accurate, with a certain course keeping function in a short time and meter-level positioning accuracy in a short time.

After the pure inertial mode (that is, GPS fusion has never been performed after power-on, and if it loses lock again after fusion, it belongs to the integrated navigation mode) is started, it has accurate attitude measurement function, can output the pitch and roll heading, and the pure inertial mode can find the north statically.

Size:

Fiber Optic Inertial Measurement Unit , Closed Loop Fiber Optic Gyroscope 0

Tags:

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable

products details

Fiber Optic Inertial Measurement Unit , Closed Loop Fiber Optic Gyroscope

Fiber Optic Inertial Measurement Unit , Closed Loop Fiber Optic Gyroscope

Fiber Optic Inertial Measurement Unit

Closed Loop Fiber Optic Gyroscope

32V DC Fiber Optic Accelerometer

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