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High Precision Laser Strapdown Inertial Navigation System Based On 3 Axis Laser Gyroscope

Categories Electronic Gyroscope Sensor
Brand Name: Kacise
Model Number: KsINS-90L
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
Delivery Time: 5-8 working days
Packaging Details: each unit has individual box and all boxes are packed in standard packages or customers requests available
Power consumption: ≤ 40W
weight: 15kg
Operating temperature: -40℃~ +65℃
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High Precision Laser Strapdown Inertial Navigation System Based On 3 Axis Laser Gyroscope

KsINS-90L type laser strapdown inertial navigation system

product description:

The KsINS-90L -type inertial navigation system is a standard high-precision laser strapdown inertial navigation system. It has the advantages of small size, light weight, high precision, and good reliability. It can meet the needs of long-term autonomous navigation in complex environments and is suitable for In various short-term navigation, integrated navigation, guidance and control and other fields. The heading alignment accuracy is better than ≤0.3mil (1σ), and the pure inertial navigation accuracy is better than 0.5nmile/h (CEP). The system can integrate satellite, radio, barometric altimeter, Doppler, odometer and other information to achieve high-precision integrated navigation.

Features:

● 15kg lightweight high-precision laser strapdown product, 40% cheaper than traditional products

●Using domestic high-precision spatial three-axis laser gyroscope and quartz flexible accelerometer

●Space three-axis laser gyroscope bias stability is better than 0.001°/h (1σ)

●Accelerometer bias stability is better than 30μg (1σ)

●Achieve static and dynamic base alignment, and can choose self-alignment, on-the-fly alignment or transfer alignment according to user needs

●It can be integrated with various information such as satellites, odometers, altimeters, star sensors, etc. for combined navigation, and the interface has strong scalability


Application fields and application modes:

Land use, navigation, drones, and can also be extended to other applications.


System performance:

Car navigationship navigationDrone navigationShip local datum
Location (CEP)

≤ 0.05%D,

Odometer assist

≤ 0.1m,

Differential Satellite Assist

≤ 1nm/24h,

Trip meter assist

≤ 0.1m,

Differential Satellite Assist

≤ 0.5nmile/h≤ 1m (relative)
Speed(1σ)≤ 0.2m/s≤ 0.6m/s≤ 0.6m/s≤0.2m/s(relative)
Heading(1σ)≤ 0.3mil≤0.1mil (relative)
Attitude (1σ)≤ 0.02°≤ 0.01° (relative)
Align time5min15-20min5min5min

System features:

Power consumption≤ 40W
size300mm (L) × 250mm (W) × 220mm (H)
weight15kg
Input voltage18V~32V
Operating temperature-40℃~ +65℃
Mechanical environmentimpactHalf sine wave 30g, 11ms
vibrationGJB150.16A-2009.C.3
Interface information

RS-422×2; RS-232×1;

Ethernet interface; CAN bus interface;

Odometer interface×1;Altimeter interface;Speedometer interface


Device performance:

TopAccelerometer
Bias stability≤ 0.001°/h,1σOffset Repeatability≤ 30μg, 1σ
Offset Repeatability≤ 0.001°/h,1σBias stability≤ 30μg, 1σ
scaling factor≤ 5ppm, 1σScaling factor repeatability≤ 50ppm, 1σ
random walk≤ 0.0005°/ , 1σScale factor stability≤ 50ppm, 1σ

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