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Small Volume Strapdown Inertial Navigation System Uses Optical Fiber Gyroscope For UAV

    Buy cheap Small Volume Strapdown Inertial Navigation System Uses Optical Fiber Gyroscope For UAV from wholesalers
     
    Buy cheap Small Volume Strapdown Inertial Navigation System Uses Optical Fiber Gyroscope For UAV from wholesalers
    • Buy cheap Small Volume Strapdown Inertial Navigation System Uses Optical Fiber Gyroscope For UAV from wholesalers
    • Buy cheap Small Volume Strapdown Inertial Navigation System Uses Optical Fiber Gyroscope For UAV from wholesalers

    Small Volume Strapdown Inertial Navigation System Uses Optical Fiber Gyroscope For UAV

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    Brand Name : Kacise
    Model Number : KsINS-B
    Certification : certificate of explosion-proof, CE
    Payment Terms : T/T, Western Union, MoneyGram
    Supply Ability : 1000 Pieces per Week
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    Small Volume Strapdown Inertial Navigation System Uses Optical Fiber Gyroscope For UAV

    KsINS-B optical fiber strapdown inertial navigation system

    product description:

    The KsINS-B optical fiber strapdown inertial navigation system is a small general-purpose inertial navigation system using 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, 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: 2~5nmile/30min (CEP)

    Integrated navigation with satellite: height 10m; level 5m

    Speed accuracyIn integrated navigation mode: sky speed ≤ 0.3m/s, horizontal speed ≤ 0.2m/s
    heading alignment accuracy

    ≤ 1.0° (1σ) (self-aligned)

    ≤ 0.1° (1σ) (dual antenna positioning, baseline 2 meters)

    Heading maintenance accuracy0.2° /h (pure inertia), 0.1° (integrated navigation)
    Attitude alignment accuracy0.05° (1σ)
    Attitude maintenance accuracy0.1° (pure inertia), 0.05° (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:

    Dimensions135mm×135mm×84mm
    Installation dimensions

    No shock absorption: M6 screw 121mm×121mm

    With shock absorption: M4 screw 121mm×121mm

    weight≤ 2.1kg
    waterproof levelIP67

    External Interface:

    powered by18V~36V DC
    Power consumption≤ 11W
    Input/output interface

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

    LVTTL interface 1 CAN×2, network port×1,

    Pulse interface × 2, data storage 8G

    Data output frequency≤1000Hz

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