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FG-900M UAV USE FIBER OPTIC INERTIAL NAVIGATION SYSTEM FAST ALIGN LESS THAN ONE MINUTE

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FG-900M UAV USE FIBER OPTIC INERTIAL NAVIGATION SYSTEM FAST ALIGN LESS THAN ONE MINUTE

Name: FG900M UAV USE FIBER OPTIC INERTIAL NAVIGATION SYSTEM FAST ALIGN LESS THAN ONE MINUTE
Brand: THUNDSEA
Price: 1 USD

Brand Name : THUNDSEA

Model Number : FG-900M

Certification : CCS

Place of Origin : Qingdao

MOQ : one set

Payment Terms : L/C, T/T

Supply Ability : 30 set per month

Delivery Time : 15 Days

Packaging Details : carton box

Align time : ≤1 min

Gyro bias stability : 0.5°/h(RMS)

Gyro bias repeatability : 0.5°/h(RMS)

Accelerometer bias stability : 0.5°/h(RMS)

Accelerometer bias repeatability : 0.5°/h(RMS)

Angular rate : ±500°/s

Acceleration : ±30g

Temperature : ﹣40℃~60℃

Shock : 20g,11m/s

Vibration : 6.0g@10~2000HZ@≤1

MTBF : 5000h

Power Supply/Consumption : 28V DC/10W

Interface : RS422

Dimension : Φ90×120mm

Weight : ≤1.2kg

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FG-900M UAV USE FIBER OPTIC INERTIAL NAVIGATION SYSTEM FAST ALIGN LESS THAN ONE MINUTE

Overview

The tactical FOG inertial measurement unit which has the functions of angular rate and acceleration input/output,error compensation,etc.is composed of inertial sensor assembly,electric circuits and chassis.it can provide angular rate and acceleration for flight control system and stabilized control system,which is suite for short distance guided missiles,UAVs,antenna stable reference system,guided rocket reconstruction,etc.

Features

● Adopt threeaxis closed-loop FOG as the core component

● Low cost,small volume,light weight

● Low power consumption

● High reliability

Application

Short distance guided missiles,Guided rockets,UAVs,Antenna stable reference system etc.

The Tactical FOG Strapdown Inertial Measurement Unit

Specifications

Accuracy	Fast Align time	≤1 min
	Gyro bias stability	0.5°/h(RMS)
	Gyro bias repeatability	0.5°/h(RMS)
	Accelerometer bias stability	0.5°/h(RMS)
	Accelerometer bias repeatability	0.5°/h(RMS)
Dynamic range	Angular rate	±500°/s
Dynamic range	Acceleration	±30g
Operation requirement	Temperature	﹣40℃~60℃
	Shock	hail-sine wave 20g,11m/s
	Vibration	amplitude of vibration(peak value) 6.0g
		frequency domain 10~2000Hz
		sweep rate ≤1 oct/min
MTBF		5000h
Power Supply/Consumption		28V DC/10W
Interface		RS422
Dimension		Φ90×120mm
Weight		≤1.2kg

FG-900M UAV USE FIBER OPTIC INERTIAL NAVIGATION SYSTEM FAST ALIGN LESS THAN ONE MINUTE

Product Tags:

1 min irs inertial reference system

0.5°/h inertial navigation unit

0.5°/h imu inertial measurement unit

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