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

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

Miniature Inertial Navigation System

UAV Inertial Navigation System

Fiber Optic Gyro Inertial Navigation System

Place of Origin:

China (Mainland)

Hàng hiệu:

Kacise

Chứng nhận:

certificate of explosion-proof, CE

Model Number:

KsINS-II

Liên hệ với chúng tôi
Yêu cầu Đặt giá
Chi tiết sản phẩm
Align time:
≤5min
heading alignment accuracy:
≤ 0.06° (1σ) (self-aligned)
Working/storage temperature(℃):
-40℃ ~+60℃ /-45℃ ~+80℃
Làm nổi bật:

Miniature Inertial Navigation System

,

UAV Inertial Navigation System

,

Fiber Optic Gyro Inertial Navigation System

Điều khoản thanh toán và vận chuyển
Minimum Order Quantity
1pcs
Packaging Details
each unit has individual box and all boxes are packed in standard packages or customers requests available
Payment Terms
T/T, Western Union, MoneyGram
Supply Ability
1000 Pieces per Week
Sản phẩm liên quan
Liên hệ với chúng tôi
86--17719566736
Liên hệ ngay bây giờ
Mô tả sản phẩm

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.

Miniature Inertial Navigation System With High Precision Fiber Optic Gyro For UAV Navigation 0

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 accuracy Pure inertia: 1nmile/h (CEP); integrated navigation with satellite: altitude 10m; horizontal 5m
Speed accuracy In integrated navigation mode: sky speed ≤ 0.2m/s, horizontal speed ≤ 0.1m/s
heading alignment accuracy ≤ 0.06° (1σ) (self-aligned)
Heading maintenance accuracy 0.01° /h (pure inertia), 0.02° (integrated navigation)
Attitude alignment accuracy 0.01°(1σ)
Attitude maintenance accuracy 0.02° (pure inertia), 0.01° (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 160mm×160mm×140mm
weight ≤ 4.0kg
waterproof level IP67

 

External Interface:

powered by 18V~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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