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Inertial Measurement Unit Integrating Three Accelerometers And Gyroscope And Inclinometer

    Buy cheap Inertial Measurement Unit Integrating Three Accelerometers And Gyroscope And Inclinometer from wholesalers
     
    Buy cheap Inertial Measurement Unit Integrating Three Accelerometers And Gyroscope And Inclinometer from wholesalers
    • Buy cheap Inertial Measurement Unit Integrating Three Accelerometers And Gyroscope And Inclinometer from wholesalers
    • Buy cheap Inertial Measurement Unit Integrating Three Accelerometers And Gyroscope And Inclinometer from wholesalers
    • Buy cheap Inertial Measurement Unit Integrating Three Accelerometers And Gyroscope And Inclinometer from wholesalers
    • Buy cheap Inertial Measurement Unit Integrating Three Accelerometers And Gyroscope And Inclinometer from wholesalers

    Inertial Measurement Unit Integrating Three Accelerometers And Gyroscope And Inclinometer

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    Brand Name : KACISE
    Model Number : STIM300
    Certification : CE
    Payment Terms : T/T, Western Union, MoneyGram
    Supply Ability : 1000 Piece/Pieces per Week negotiable
    Delivery Time : 5-8 work days
    • Product Details
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    Inertial Measurement Unit Integrating Three Accelerometers And Gyroscope And Inclinometer

    Inertial Measurement Unit STIM300

    1 FEATURES:

    ● Miniature package

    ● Low noise

    ● Low bias instability

    ● Excellent performance in vibration and shock environments

    ● 9 axes offered in same package

    ● Electronically calibrated axis alignment

    ● Gyros based on Safran ButterflyGyroTM

    ● Single-crystal silicon technology

    ● No intrinsic wear-out effects

    ● High stability accelerometers and inclinometers

    ● Insensitive to magnetic fields

    ● Full EMI compliance

    ● Digital interface, RS422

    ● Fully configurable

    ● Continuous self-diagnostics

    ● RoHS compatible


    2 GENERAL DESCRIPTION

    STIM300 is an IMU consisting of 3 high accuracy MEMS-based gyros, 3 high stability accelerometers and 3 high stability inclinometers in a miniature package. Each axis is factory-calibrated for bias, scale factor and compensated for temperature effects to provide high-accuracy measurements in the temperature range -40°C to +85°C. The unit runs off a single +5V supply.

    STIM300 communicates via a standard high-level RS422 interface. The use of a 32-bit RISC ARM microcontroller provides flexibility in the configuration, like choice of output unit, sample rate, low pass filter -3dB frequency and RS422 bit-rate and protocol parameters. All configurable parameters can be defined when ordering or set by customer.

    When STIM300 is powered up, it will perform an internal system check and synchronize the sensor channels. As an acknowledgement of the complete power-up sequence, it will provide special datagrams containing part number, serial number, configuration and bias trim data. STIM300 will then automatically proceed to provide measurement data.

    The measurement data is transmitted as packages of data on a fixed format (datagram) at intervals given by the sample rate together with a synchronization signal (TOV). The datagram is in binary coded format in order to have an efficient transfer of data. In addition to the measurement data itself, the datagram contains an identifier, status bytes and a 32 bit CRC (Cyclic Redundancy Check) to provide high degree of fault detection in the transmissions. The status bytes will flag any detected errors in the system. STIM300 can also be configured to transmit data only when triggered by a separate digital input signal (ExtTrig).

    For more advanced users, the gyro may be put in Service Mode. In this mode all the configuration parameters can be intermediately or permanently changed by overwriting the current settings in the flash memory. In Service Mode the commands and responses are in a human readable format (ASCII); to enable the use of terminal-type software during typical product integration. Service Mode also provides the ability to perform single measurements, perform diagnostics and obtain a higher detail level of detected errors reported in the status bytes.

    Finally, STIM300 may be put in Utility Mode. This mode is similar to Service Mode, but made for machine-machine communication.


    3 BLOCK DIAGRAM:

    4 ABSOLUTE MAXIMUM RATINGS

    Stresses beyond those listed in Table 4-1may cause permanent damage to the device.

    Exposure to any Absolute Maximum Rating condition for extended periods may affect device reliability and lifetime.

    Table 4-1: Absolute maximum ratings


    ParameterRatingComment

    Mechanical shock

    ESD human body model Storage temperature

    VSUP to GND

    RxD+ or RxD- to GND

    RxD+ to RxD-

    TxD+ or TxD- to GND

    ExtTrig to GND

    TOV to GND

    NRST to GND

    AUX+ to AUX-

    AUX+ or AUX- to GND Chassis to GND

    Helium sensitivity

    1 500g/0.5ms half-sine

    ±2kV

    -55°C to +90°C

    -0.5 to +7V

    -0.3V to +7V

    ±6V

    -8V to +8V

    -0.3V to +7V

    -0.3V to +7V

    -0.3V to +7V

    ±6.5V

    ±6.5V

    500VDC

    Any direction. Ref: MIL STD-883G

    Ref: JEDEC/ESDA JS-001

    Up to 1000 hours


    with 120Ω Line Termination = ON


    Not to be exposed to helium concentrations higher than those normally found in the atmosphere


    5 SPECIFICATIONS

    Table: Operating conditions


    ParameterConditionsMin Nom MaxUnitNote
    INPUT RANGE, ANGULAR RATE±400°/s
    INPUT RANGE, ACCELERATION±10g1
    INPUT RANGE, INCLINATION±1.7g
    POWER SUPPLY4.5 5.0 5.5V2,3
    OPERATING TEMPERATURE-40 +85°C

    Note 1: Other ranges available, ref.Table 5-4(5g),Table 5-6(30g) andTable 5-7(80g)

    Note 2: At supply voltages above 5.85V (nominal value) an internal voltage protection circuit will cut power and the unit will go into reset until the voltage is back within operating conditions.

    Note 3: At supply voltages below 4.05V (nominal value) the unit will go into reset until the voltage is back within

    operating conditions. Due to power consumption being much lower in reset compared to normal operation, the series resistance between power source and STIM300 could give rise to an oscillating behavior of the input

    voltage to the unit.


    Table: Functional specifications, general


    ParameterConditionsMin Nom MaxUnitNote

    POWER CONSUMPTION

    Power consumption

    1.5 2W
    TIMING
    Start-Up time after Power-On0.3s1
    Time to transmit after Reset0.2s2
    Time to valid dataT=+25°C

    0.7

    1

    s

    s

    3

    3

    RS422 Bit-Rateref.Table 5-11
    RS422 Bit-Rate Accuracy±1%4

    RS422 PROTOCOL

    Start Bit

    Data Length

    Parity

    Stop Bits

    1

    8

    None

    1

    bit

    bits

    bit


    5

    5

    RS422 LINE TERMINATION
    Input resistanceLine termination = ON120Ω
    Input resistanceLine termination = OFF48 125
    RESET (NRST PIN)
    Logic levels

    “high”

    “low”

    2.3

    0.6

    V

    V

    Minimum hold time for reset1µs
    Pull-Up Resistor80 100
    EXTERNAL TRIGGER (ExtTrig
    PIN)
    Logic levels

    “high”

    “low”

    2.3

    0.6

    V

    V

    TriggerNegative transition
    Time between triggers

    Measurement unit:

    angular rate

    incremental angle

    average rate

    integrated angle

    0.5 127

    0.5 127

    0.5 65

    0.5 8


    ms

    ms

    ms

    ms

    6,7

    6,8

    6,9

    6, 10

    Minimum “high” time before

    trigger, text_hi

    250ns11
    Minimum “low” time after trigger, text_lo250ns11

    Delay from external trigger to start of transmission, text_dl

    Pull-Up Resistor

    Latency

    86

    40 50

    1000

    µs

    µs

    11

    TIME OF VALIDITY (TOV PIN)

    Output configuration

    VOH


    VOL

    TOV active level

    Minimum time of TOV, ttov_min Delay from internal time-tick to TOV active, ttov_dl

    Delay from TOV active (to start of transmission, ttx_dl


    5V logic: IOH = - 10 µA

    5V logic: IOH = - 100 µA 3.3V logic: IOH = - 10 µA 3.3V logic: IOH = - 100 µA IOL = 10 mA

    Open drain with internal pull up

    0.9 VSUP

    0.7 VSUP

    0.6 VSUP

    0.47 VSUP

    0.1

    Active “low”

    50

    1.2 6

    80


    V

    V

    V

    V

    V

    µs

    µs

    µs


    12

    12

    12

    12


    13

    13

    13

    CHASSIS

    Isolation resistance chassis to GND (pin 15)

    500VDC100

    Note 1: Time from Power-On to start of datagram transmissions (starting with part-number datagram)

    Note 2: Time from Reset release to start of datagram transmissions (starting with part-number datagram)

    Note 3: Time from Power-On or Reset to the reset of the Start-Up bit (Bit 6 in the STATUS byte ref.Table 5-23). During this period the output data should be regarded as non-valid.

    Note 4: If a user-defined bit-rate larger than 1.5Mbit/s is used, the deviation may exceed the specification due to the resolution of the bit-rate generator, ref. section9.13.1

    Note 5: Other values can be configured, ref.Table 5-11

    Note 6: If time between triggers is longer than 127ms, the sample counter will over-run

    Note 7: Time between triggers should be carefully evaluated as long time between triggers in combination with high bandwidths could lead to issues related to folding. Similar for accelerometer and inclinometer outputs

    Note 8: If time between triggers is longer than 8ms, an overload may occur in the incremental angle. An overload will be flagged in the status byte, ref.Table 5-23. Similar for accelerometer and inclinometer outputs

    Note 9: If time between triggers is longer, the accuracy of average rate may also be reduced. Similar for accelerometer and inclinometer outputs

    Note 10: If time between triggers is longer, the integrated angle may have wrapped several times and hence the

    change in angle from last sample will not be possible to calculate. Similar for accelerometer and inclinometer

    outputs

    Note 11: For definition, ref.Figure 7-3

    Note 12: Digital output level can be configured to 5V or 3.3V in SERVICEMODE (ref. section9.7) or when ordering (ref. section12)

    Note 13: For definition, ref.Figure 7-4andFigure 7-5


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