Optical Fiber Rotating Inertial Navigation System For UAV Flight Control And Navigation And Positioning

Brand Name:Kacise
Certification:certificate of explosion-proof, CE
Model Number:KsINS-G107A
Minimum Order Quantity:1pcs
Payment Terms:T/T, Western Union, MoneyGram
Place of Origin:China (Mainland)
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Address: i City, No11, TangYan South road, Yanta District, Xi'an,Shaanxi,China.
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Product Details

KsINS-G107A fiber optic rotating inertial navigation system

product description:

KsINS-G107A is a single-axis rotating inertial navigation system that uses high-precision fiber optic gyroscopes and quartz flexible accelerometers to suppress navigation error divergence through rotational modulation. It is equipped with a set of satellite receivers by default and has differential positioning and dual-antenna measurement capabilities. It has directional and multi-channel integrated navigation capabilities; the system uses information fusion algorithms to judge the validity of satellite navigation information, timely distinguish deception signals, and support aircraft to safely escape from deception areas. It has astronomical navigation and visual navigation software and hardware interfaces to meet UAV attitude control and navigation and positioning requirements.

Features:

● High reliability, light weight, long endurance and high precision navigation

● Rich and flexible combined navigation modes, smooth switching between modes, and fault-tolerant navigation capabilities

● Adapt to a variety of starting conditions, and can quickly respond to power outages and restarts

● Good vibration-shock-heat composite environmental adaptability

● Have complete BIT design


Application fields and application modes:

It can be applied to all types of large and medium-sized long-endurance UAVs.


Performance indicators :

Align timeNormal alignment on the ground: ≤ 5min
Emergency alignment: ground alignment 30s + air alignment 10min

Position Accuracy (CEP)

Pure inertia: 1.5 nmile/6h

After 15min of inertial/satellite combination: 1.0 nmile/6h

Inertia/satellite combination: ≤ 10m

Speed Accuracy (RMS)Pure inertia ≤ 1m/s (6h); inertia/satellite combination ≤ 0.2m/s
Attitude angle accuracy (RMS)Pure inertia ≤ 0.02° (6h); inertia/satellite combination ≤ 0.02°
Heading angle accuracy (RMS)Pure inertia ≤ 0.05° (6h); inertia/satellite combination ≤ 0.05°

Application environment :

Working/storage temperature(℃)-55℃ ~+70℃
Dynamic RangeAngular velocity: ±300°/s, acceleration: -30g ~ +30g
Mechanical propertiesShock environment: half sine wave 20g, 11ms; vibration environment: typical drone vibration environment

Physical properties:

Dimensions175mm×216mm×175mm
Installation method

Direct mounting (waist mounting) or optional bracket mounting

(bottom installation)

Installation dimensions

Bracket installation size: 224mm×220mm

(Installation through hole: Φ8.5mm)

weightHost ≤ 7.0kg; bracket (optional) ≤ 1.5kg or customized ≤ 1.5kg or customized

External Interface:

powered byPower supply 18V~36V DC, power consumption ≤ 32W

Input/output interface

7 channels RS-422, 1 channel RS-232;

2 channels CAN (FD); 1 channel 1M 1553B;

1 channel 4M1553B

Data output frequency200Hz (typical)

China Optical Fiber Rotating Inertial Navigation System For UAV Flight Control And Navigation And Positioning supplier

Optical Fiber Rotating Inertial Navigation System For UAV Flight Control And Navigation And Positioning

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