Fiber Optical Inertial Guidance System 21.215.512.5cm Highly Reliable

Browse Categories

Wuhan Liocrebif Technology Co., Ltd

City: wuhan

Province/State:hubei

Country/Region:china

Tel:86--159-1069-1166

Contact Person:
Mrs.Shirley View Contact Details

Fiber Optical Inertial Guidance System 21.215.512.5cm Highly Reliable

Fiber Optical Inertial Guidance System 21.2*15.5*12.5cm Highly Reliable

Brand Name	Liocrebif
Model Number	LKF-FSI400
Certification	GJB 9001C-2017
Place of Origin	China
Minimum Order Quantity	1
Price	5000-25000CHY
Payment Terms	T/T
Supply Ability	10000
Delivery Time	2-4 weeks
Packaging Details	Wooden box/Cardboard box/Container
Color&Classification	LKF-FSI400
Dimensions	21.215.512.5cm
Module Type	Gyroscope
Brand	LIOCREBIF
Application	Mobile measurement of position and attitude reference, Unmanned vehicles, unmanned ships/boats, Surveying and mapping, Stable platforms Underwater vehicles, Motion communication, Intelligent driving, Airborne control, Intelligent mining North seeking
Original Place	China

Detailed Product Description

Essential details

MOQ:1

Size:L(21.2)*W(15.5)*H(12.5) cm

Specification Number:LKF-FSI400

Product Introduction

Introduction

The FSI400 Fiber-Optic Gyro-Inertial/Satellite Integrated Navigation System is a highly reliable and cost-effective navigation system suitable for a wide range of applications, including navigation, control, and measurement in fields such as aircraft, unmanned vehicles, unmanned boats, and drones.
The integrated navigation system adopts the modular design philosophy of similar products, incorporating high-precision closed-loop fiber optic gyroscopes (FOG) and high-precision accelerometers, combined with high-performance GNSS boards. The hardware circuitry is designed using an FPGA+DSP architecture. Through multi-sensor fusion algorithms, GPS position and velocity data are input into the filter, while INS position, velocity, and attitude data are also used as filter inputs. The filter compares the differences between the two sets of data to establish an error model for estimating INS errors, and uses these errors to correct the inertial navigation results, thereby obtaining the combined navigation results for velocity, position, and attitude. The inertial navigation system offers different configuration modes to suit various platforms, such as airborne, vehicle-mounted, and ship-mounted applications. When vehicle-mounted, vehicle constraints are incorporated. Through error estimation and correction, the system achieves long-term high-precision navigation and positioning functionality for the platform.

Technical Specification

The integrated navigation system integrates high-precision fiber optic gyroscopes and accelerometers within an independent structure. The gyroscopes and accelerometers selected for the system represent the leading level of process inertial components in the industry. The system has undergone full temperature parameter compensation for zero position, scale factor, non-orthogonal error, and acceleration-related items, enabling it to maintain high measurement accuracy over extended periods.
The series of integrated navigation systems can be customized with different hardware and software configurations to meet user requirements. For specific navigation applications, the gyroscope can be replaced with a high-precision gyroscope to maximize flexibility and meet the diverse needs of different users.

Table 1 Performance parameters of LKF-FSI400

Fiber Optical Gyroscope
Range (°/s)	±300
Zero offset (°/h)	0.01
Zero offset stability (°/h, 10s)	0.01
Zero offset instability (°/h, Allan)	0.001
Zero offset repeatability (°/h, 6 power-ups)	0.01
Angular random walk (°/√h)	0.0005
Scale nonlinearity (ppm)	10
Scale asymmetry (ppm)	10
Scale repeatability (ppm)	10
Cross-coupling (rad)	≤0.001
Bandwidth (Hz)	≥200
Quartz accelerometer
Range (g)	±20
Zero position (mg, 1σ)	≤ 0.1
Zero offset stability (ug, 10s smoothing)	10
Zero bias stability (ug, Allan)	5
Zero bias repeatability (ug)	10
Velocity random walk (mm/s/√h)	5
Scale factor nonlinearity (mg, ppm)	5
Cross-coupling (rad)	10
Bandwidth (Hz)	≥200
Pure inertial navigation accuracy
Self-alignment accuracy (°, 1σ)	0.06
Attitude alignment accuracy (°, 1σ)	0.005
Heading hold (°, 1σ)	0.06
Attitude hold (°/h, 1σ)	0.03
Horizontal velocity (m/s, 1σ)	＜0.3
Pure inertial navigation accuracy (1σ)	＜1n mile/h
Depth measurement accuracy (cm)	5
Inertial/odometer combination accuracy	≤0.002D
Combined navigation accuracy
Combined heading accuracy (°, 1σ, real-time)	0.03
Combined horizontal attitude (°, 1σ, real-time)	0.01
Combined heading accuracy (°, post-processing)	0.003
Combined horizontal attitude (°, post-processing)	0.001
Combined horizontal position (m, 1σ)	3(Single Point),0.02+1ppm(RTK)
Combined vertical position (m, 1σ)	5(Single Point),0.03+1ppm(RTK)
Combined horizontal velocity (m/s, 1σ)	0.1
Combined vertical velocity (m/s, 1σ)	0.15
Satellite receiver
Timing accuracy	20ns
Positioning time	≤40s
Start-up time	≤2s
Positioning data update rate	10Hz
Operating altitude	10000m
Satellite mode	GPS:L1/L2/L5； BeiDou:B1/B2/B3； GLONASS:L1/L2.
Electrical/mechanical interface
Input voltage	12～36VDC(Suggest 24V)
Power consumption	≤18W
Dimensions	212 × 155 × 125 mm
Weight	≤5kg
Operating environment
Operating temperature	-40°C ~ +70°C
Storage temperature	-55°C ~ +85°C
Vibration	6 g @ 20~2000 Hz
Shock	100 g, 11 ms
Reliability/suitability
MTBF/MTTR	10000 h / 0.5 h
Maintenance	BIT 95%

Main Features

Domestic core components, high performance, modular, low weight
Supports full GNSS frequency points, high positioning and orientation accuracy in complex environments
Rich interfaces and isolation measures
Steady-state power consumption of 18W
Full temperature calibration compensation from -45°C to +65°C
Combined navigation products support automatic north seeking, with accuracy better than 1 mil°
Built-in adaptive navigation algorithm

Application

Mobile measurement of position and attitude reference
Unmanned vehicles, unmanned ships/boats
Surveying and mapping
Stable platforms
Underwater vehicles
Motion communication
Intelligent driving
Airborne control
Intelligent mining North seeking

Fig. 1 Dimensions of the external structure

Product Tags: Fiber Optical Inertial Guidance System Highly Reliable Inertial Guidance System Highly Reliable inertial navigation unit

Related Products

MEMS Inertial Navigation System Integrated 8.3*6.6*2.4cm For North Seeker Application for sale


From:	Enter your Email please. Your email is incorrect!
To:	Wuhan Liocrebif Technology Co., Ltd
Subject:	Subject is empty!
Message:	Characters Remaining: (80/3000) Please enter 20 to 3000 characters to contact this supplier!

Fiber Optical Inertial Guidance System 21.215.512.5cm Highly Reliable

Fiber Optical Inertial Guidance System 21.215.512.5cm Highly Reliable

MEMS Inertial Navigation System Integrated 8.36.62.4cm For North Seeker Application

Fiber Optical Inertial Guidance System 21.215.512.5cm Highly Reliable

High Precision Inertial Navigation Sensors MEMS Integrated Navigation System For Vehicles

High Accuracy Ships Inertial Navigation System Widely Used Mems Inertial Navigation System

Fiber Optical Inertial Guidance System 21.2*15.5*12.5cm Highly Reliable

Fiber Optical Inertial Guidance System 21.2*15.5*12.5cm Highly Reliable

MEMS Inertial Navigation System Integrated 8.3*6.6*2.4cm For North Seeker Application

Fiber Optical Inertial Guidance System 21.2*15.5*12.5cm Highly Reliable

High Precision Inertial Navigation Sensors MEMS Integrated Navigation System For Vehicles

High Accuracy Ships Inertial Navigation System Widely Used Mems Inertial Navigation System

Fiber Optical Inertial Guidance System 21.215.512.5cm Highly Reliable

Fiber Optical Inertial Guidance System 21.215.512.5cm Highly Reliable

MEMS Inertial Navigation System Integrated 8.36.62.4cm For North Seeker Application

Fiber Optical Inertial Guidance System 21.215.512.5cm Highly Reliable