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Miniature Inertial Navigation System With High Precision Fiber Optic Gyro For UAV Navigation

Categories Electronic Gyroscope Sensor
Brand Name: Kacise
Model Number: KsINS-II
Certification: certificate of explosion-proof, CE
Place of Origin: China (Mainland)
MOQ: 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
heading alignment accuracy: ≤ 0.06° (1σ) (self-aligned)
Working/storage temperature(℃): -40℃ ~+60℃ /-45℃ ~+80℃
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Miniature Inertial Navigation System With High Precision Fiber Optic Gyro For UAV Navigation

KsINS-II fiber optic strapdown inertial navigation system

product description:

The KsINS-II optical fiber strapdown inertial navigation system is a miniaturized and general-purpose inertial navigation system using high-precision 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, high precision, good production technology and high reliability

● Using dual-board working mode, 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

● Nationally produced products

Application fields and application modes:

It can be used in the fields of high-altitude airships, rotary-wing UAVs, and fixed-wing UAVs.


Performance indicators :

Align time≤5min
Position accuracyPure inertia: 1nmile/h (CEP); integrated navigation with satellite: altitude 10m; horizontal 5m
Speed accuracyIn integrated navigation mode: sky speed ≤ 0.2m/s, horizontal speed ≤ 0.1m/s
heading alignment accuracy≤ 0.06° (1σ) (self-aligned)
Heading maintenance accuracy0.01° /h (pure inertia), 0.02° (integrated navigation)
Attitude alignment accuracy0.01°(1σ)
Attitude maintenance accuracy0.02° (pure inertia), 0.01° (integrated navigation)

Application environment :

Working/storage temperature(℃)-40℃ ~+60℃ /-45℃ ~+80℃
MTBF(h)30000h
Dynamic RangeAngular 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:

Dimensions160mm×160mm×140mm
weight≤ 4.0kg
waterproof levelIP67

External Interface:

powered by18V~36V DC
Power consumption≤ 18W

Input/output interface

RS-422×4 (multiplex), RS-232×3 (multiplex),

CAN (FD)×2 network port×1, pulse interface×2, data storage 8G, USB×1

Data output frequency≤1000Hz

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