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Attitude Heading Reference System Microelectromechanical Systems Small Volume and Weight|selectable Interface|high Accuracy|static|dynamnic|proven Technology|used In Demanding Conditions for Unmanned Aerial Vehicle (MEMS AHRS)

  • Description
Product Detail

    Attitude Heading Reference System Microelectromechanical Systems Small Volume And Weight|selectable Interface|high Accuracy|static|dynamnic|proven Technology|used In Demanding Conditions For Unmanned Aerial Vehicle (MEMS AHRS)


    1. Brief introduction


    TY421 type MEMS AHRS is R & D by the Xi'an Jierui. This product uses MEMS gyro and MEMS accelerometer, as well as a mature attitude calculation algorithm, can autonomously complete the attitude calculation function in harsh environmental conditions, can also provide heading by being combined with dual antenna GPS or magnetometer. And the combination of dual antenna GPS can continuously and real-time provide the instant position (longitude and latitude), velocity, acceleration, heading and attitude of the aircraft.


    2. Features


    (1) Auto-output  of navigation information

    (2) Meet the requirement of accurate measurement of attitude angle of aircraft, when in large maneuver flight and hovering.

    (3) Small volume and weight.

    (4) Communication interface RS422?CAN, to be selectable.

    (5) Wide voltage input range.

    (6) Can complete redevelopment according to customers’ requirement.


    3. Performances


    Sr. No.

    Item

    Grade

    Remark

     System

    1

    Preparation time

    =2min

    2

    Attitude accuracy

    =1°   1(static)

    =2°   1s (dynamic)

    3

    Heading accuracy

    =0.2°/ Baseline(GPS combined)

    =0.5°Magnetometer combined

    4

    Height accuracy

    10 m (GPS combined)

    5

    Horizontal position accuracy

    10m (CEP)(GPS combined)

    6

    Velocity accuracy

    0.02m/s  (GNSS combined)

    Environment suitability

    7

    Shock

    30g

    8

    Working temperature

    -40?~65?

    9

    Vibration

    Meet the vehicle vibration requirement of GJB150.16A-2009

    Physics characteristics

    10

    Size

    150*110*50mm

    11

    Weight

    <700g

    12

    Power supply

    18VDC~36VDC

    13

    Working power dissipation

    10W

    Interface characteristics

    14

    Interface

    RS232?RS422?CAN

    Selectable

    15

    MTBF

    =1500h


    16

    Data refresh rate

    100Hz


    17

    Band rate

    115200bps


    18

    Memory

    32G

    customized

                          

    4. Applications


    (1) Unmanned aerial vehicle

    (2) Unmanned surface vessel

    (3) Counter-terrorism, search for and rescue.

    (4) Robots, unmanned vehicles

    201706151129438882912.jpg


    5. Packages


    inertial navigation system package.jpg  inertial navigation packing.jpg



    E-mail: info@gyro-nav.com


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Inertial Navigation Systems | JieRui

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