Xi'an Kacise Optronics Co.,Ltd.

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Fiber Strapdown Inertial Navigation System For High Altitude Airships And Fixed Wing UAVs

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Xi'an Kacise Optronics Co.,Ltd.
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Province/State:Shaanxi
Country/Region:china
Contact Person:MsEvelyn Wang
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Fiber Strapdown Inertial Navigation System For High Altitude Airships And Fixed Wing UAVs

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Brand Name :Kacise
Model Number :KsINS-nano
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
Working/storage temperature(℃) :-40℃ ~+60℃ /-45℃ ~+80℃
Position accuracy :Pure inertia: 2nmile/h (CEP); integrated navigation with satellite: altitude 10m; horizontal 5m
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KsINS-nano fiber optic strapdown inertial navigation system

product description:

KsINS-nano optical fiber strapdown inertial navigation system is a miniaturized universal inertial navigation system using high precision fiber optic gyro and quartz flexible accelerometer. The product adopts compact design.

The system can be sensitive to the angular and linear motion of the UAV carrier, and output the position, speed, heading, angular rate, and linear acceleration information of the carrier 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.

Fiber Strapdown Inertial Navigation System For High Altitude Airships And Fixed Wing UAVs

Features:

● Small size, light weight, high precision, 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: 2nmile/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 ≤ 0.1° (1σ) (self-aligned)
Heading maintenance accuracy 0.02° /h (pure inertia), 0.03° (integrated navigation)
Attitude alignment accuracy 0.02°(1σ)
Attitude maintenance accuracy 0.03° (pure inertia), 0.02° (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 175mm×140mm×110mm
weight ≤ 3.6kg
waterproof level IP67

External Interface:

powered by 18V~36V DC
Power consumption ≤ 15W

Input/output interface

RS-422×2 (multiplexing), RS-232×3 (multiplexing),

CAN×2 network port×1,

Pulse interface × 2, data storage 8G

Data output frequency ≤1000Hz

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