Small Volume Strapdown Inertial Navigation System Uses Optical Fiber Gyroscope For UAV

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Xi'an Kacise Optronics Co.,Ltd.

Province/State:Shaanxi

Country/Region:china

Tel:86--17719566736

Contact Person:
Ms.Evelyn Wang View Contact Details

Small Volume Strapdown Inertial Navigation System Uses Optical Fiber Gyroscope For UAV

Brand Name	Kacise
Model Number	KsINS-B
Certification	certificate of explosion-proof, CE
Place of Origin	China (Mainland)
Minimum Order Quantity	1pcs
Payment Terms	T/T, Western Union, MoneyGram
Supply Ability	1000 Pieces per Week
Packaging Details	each unit has individual box and all boxes are packed in standard packages or customers requests available
Align time	≤5min
Speed accuracy	In integrated navigation mode: sky speed ≤ 0.3m/s, horizontal speed ≤ 0.2m/s
Heading maintenance accuracy	0.2° /h (pure inertia), 0.1° (integrated navigation)

Detailed Product Description

KsINS-B optical fiber strapdown inertial navigation system

product description:

The KsINS-B optical fiber strapdown inertial navigation system is a small general-purpose inertial navigation system using fiber optic gyroscopes and quartz flexible accelerometers. The system can be sensitive to the angular and linear motion of the UAV carrier, and output the carrier's position, speed, heading, angular rate, and linear acceleration information in real time. It can be combined with a satellite receiver to complete integrated navigation operations, which can meet the needs of various UAVs. Attitude control, navigation and positioning requirements.

Features:

● Small size, light weight, good production technology and high reliability

● Rich communication interfaces

● The output protocol is flexible and can be configured through test software

● Vibration reduction accessories are provided to meet the needs of harsh vibration environments

● Have a complete BIT strategy and passed the actual flight assessment

Application fields and application modes:

It has been maturely used in the fields of high-altitude airships, rotary-wing UAVs, and fixed-wing UAVs.

Performance indicators :

Align time	≤5min
Position accuracy	Pure inertia: 2~5nmile/30min (CEP) Integrated navigation with satellite: height 10m; level 5m
Speed accuracy	In integrated navigation mode: sky speed ≤ 0.3m/s, horizontal speed ≤ 0.2m/s
heading alignment accuracy	≤ 1.0° (1σ) (self-aligned) ≤ 0.1° (1σ) (dual antenna positioning, baseline 2 meters)
Heading maintenance accuracy	0.2° /h (pure inertia), 0.1° (integrated navigation)
Attitude alignment accuracy	0.05° (1σ)
Attitude maintenance accuracy	0.1° (pure inertia), 0.05° (integrated navigation)

Application environment :

Working/storage temperature(℃)	-40℃ ~+60℃ /-45℃ ~+80℃
MTBF(h)	30000h
Dynamic Range	Angular velocity: ±300°/s; Acceleration: -25g~25g
Mechanical properties	Endurance shock environment: half sine wave 20g, 11ms, Endurance Vibration Environment: 1. No shock absorption: GJB150.16A-2009 Figure C.3 Rear peak sawtooth wave 2. With shock absorption: GJB1032 random vibration spectrum

Physical properties:

Dimensions	135mm×135mm×84mm
Installation dimensions	No shock absorption: M6 screw 121mm×121mm With shock absorption: M4 screw 121mm×121mm
weight	≤ 2.1kg
waterproof level	IP67

External Interface:

powered by	18V~36V DC
Power consumption	≤ 11W
Input/output interface	RS-422×3 (multiplexing), RS-232×2 (multiplexing), LVTTL interface 1 CAN×2, network port×1, Pulse interface × 2, data storage 8G
Data output frequency	≤1000Hz

Product Tags: Optical Fiber Gyroscope Inertial Navigation System Small Volume Inertial Navigation System

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