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RION/MEMS IMU with GPS output pitch roll heading acceleration and angular speed/IMU560

RION/MEMS IMU with GPS output pitch roll heading acceleration and angular speed/IMU560
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RION/MEMS IMU with GPS output pitch roll heading acceleration and angular speed/IMU560 - 1

IMU560 COMBINED INERTIAL NAVIGATION IMU COMBINED INERTIAL NAVIGATION SYSTEM ○INS&IMU TECHNICAL MANUAL ○3D compass ○Digital inclinometer ○Accelerometer ○Gyro ○North finder SINCE2008 · Inertial Attitude Measurement

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RION/MEMS IMU with GPS output pitch roll heading acceleration and angular speed/IMU560 - 2

IMU560 COMBINED INERTIAL NAVIGATION Production implementation standard reference ● Enterprise quality system standard：ISO9001:2008 standard (certification number: 128101) ● Inclination sensor production standard: GB/T 191 SJ 20873-2003 General specification for inclinometer and level ● Dip Sensor Metrology Calibration Standard: JJF1119-2004 Electronic Level Calibration Specification ● Gyro acceleration test standard: QJ 2318-92 gyro accelerometer test method ● Software Development Reference Standard: GJB 2786A-2009 General Requirements for Military Software Development ● Product...

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RION/MEMS IMU with GPS output pitch roll heading acceleration and angular speed/IMU560 - 3

IMU560 COMBINED INERTIAL NAVIGATION ○3D compass ○Digital inclinometer ○Accelerometer ○Gyro ○North finder SINCE2008 · Inertial Attitude Me

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RION/MEMS IMU with GPS output pitch roll heading acceleration and angular speed/IMU560 - 4

IMU560 COMBINED INERTIAL NAVIGATION ▶ PRODUCT DESCRIPTION The IMU560 series is a GPS/INS integrated navigation system built by RION.the inertial measurement unit (IMU) is precision calibrated throughout the temperature range to meet performance requirements in different environments. The multi-data Kalman filter fusion algorithm is realized by a built-in navigation computer, and outputs real-time accurate carrier posture, heading information, three-dimensional position and velocity information, and various inertial device information. The appearance is exquisite, the structure is small, the...

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RION/MEMS IMU with GPS output pitch roll heading acceleration and angular speed/IMU560 - 5

HEADING POSITION ESTIMATION ACCURACY MAGNETOME TER MAGNETIC AZIMUTH Air pressure Heading Accuracy 1a Pure Inertial Position Estimation Accuracy 1a Output Frequency Range Zero Bias Instability (Allan) Zero Bias Stability (10s Mean Zero Bias Repeatability Nonlinear Error Scale Factor Nonlinearity1 Scale Factor Change ( 25 ° C) Resolution Acceleration Sensitivity Angle Random Walk Noise Intensity Bandwidth Range Zero Bias Stability Full Temperature Zero Bias Scale Factor Stability Resolution Nonlinear2 Noise Intensity Bandwidth Range Range Accuracy Pressure range Barometric error Start Time...

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RION/MEMS IMU with GPS output pitch roll heading acceleration and angular speed/IMU560 - 6

IMU560 COMBINED INERTIAL NAVIGATION *Factory qualified test indicators 1. 1. Within ±100°/s, the symmetry and nonlinearity are required to be <200ppm, and the test angular 2. Measure within ±1g and full scale separately ► INSTALLATION INSTRUCTIONS Power Supply Is Dc 9-36V, Ripple <50mv, Current 0.5A At Least. If Power Noise Is Big Or Power Wire Is Long, User Better Use Filter Or Stabilizer. 1. Use M4 Half-Round Screw To Fix Imu On Carrier, If It Is Loose, The Accuracy Will Be Affected. 2. Install The Imu In The Center Of Carrier As Much As Possible. 3. Avoid Violent Vibration, Sudden...

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RION/MEMS IMU with GPS output pitch roll heading acceleration and angular speed/IMU560 - 7

IMU560 COMBINED INERTIAL NAVIGATION ▶ DIMENSION ▶ UPPER COMPUTER OF INERTIAL NAVIGATION SYSTEM 1. Function of Upper computer Software The overall view of the interface of the upper computer is as shown in the below(picture 1-1）， It mainly consists of serial port setting area, device setting area, system setting area, data saving（Save Options） 3D dynamic view , （3D model） original data area and main function area. The prompt message , moved to the column "?" is the description of each column, and the contents of each zone are introduced one by one below. (picture 1-1） ①：Serial Port Com :...

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RION/MEMS IMU with GPS output pitch roll heading acceleration and angular speed/IMU560 - 8

IMU560 COMBINED INERTIAL NAVIGATION Protocol : Mode : Connect : choose the protocol used to connect to the device； Data output mode； Confirm connection device； ③：Sersor Setting Baud : Set device baud rate； Fre. : Set device data output rate； Gravity : Set gravity level； Save : Save settings； ④：Save Path : File path Browse : Select the save file path； Save : Start saving data ⑤：Main function area waveform drawing Interface As shown in the below picture(picture 1-2)，Display real-time data waveform, the horizontal axis is the count value, the vertical axis is the data value, the left mouse...

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RION/MEMS IMU with GPS output pitch roll heading acceleration and angular speed/IMU560 - 9

IMU560 COMBINED INERTIAL NAVIGATION ® : 3D model 3D Dynamic display of equipment posture. ® : Original Data As shown in the figure above, the serial port data printing function. 2.Operating procedure Software setup interface,as shown in picture 1-2: the steps described following: (1 ) Step 1 setup: serial port setting ©After opening the software, select the corresponding port; ©Select the current verification mode of the device (NONE, EVEN Factory default NONE) ©Select the current baud rate of the device(2400, 4800, 9600, 19200, 38400, 115200, 230400 Factory default 9600) ©Click...

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RION/MEMS IMU with GPS output pitch roll heading acceleration and angular speed/IMU560 - 10

RION PROTOCOL 1. Communication frame format 1.1 Communication frame format Notes: A. LEN data length domain includes the byte number of data domain (Datas), MSB at front, LSB at back, length is 0 means no data domain, the longest data domain length is 504 bytes, the longest frame byte is 512 bytes. B. CRC calculation start from CMD command domain, including length domain and data domain, LSB at back, calculating CRC by function below: uintl6 calcCRC(const uint8 *pBuffer, uintl6 bufferSize) { ' uintl6 poly = 0x8408; uintl6 crc = 0; uint8 carry; uint8 i bits; uintl6 j; for (j = 0;...

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RION/MEMS IMU with GPS output pitch roll heading acceleration and angular speed/IMU560 - 11

IMU560 COMBINED INERTIAL NAVIGATION 2.1 normal mode In normal mode, user send inquiry or setting command, the device response accordingly. The device response has two formats: response (CMD=ASK) and reply (CMD=RET), for detail, please refer to chapter 4 command list. 2.1.1 response Response frame format as below : remarks : The error code constitutes the data domain of the frame(DATA). 2.1.2 reply The reply is a one-to-one response to the user command. The CMD and data domain of different query commands are different. Please refer to the command list in Chapter 4.0 3. Output MASK and output...

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RION/MEMS IMU with GPS output pitch roll heading acceleration and angular speed/IMU560 - 12

IMU560 COMBINED INERTIAL NAVIGATION olnclinometer_o3D compass_oDigital inclinometer_oAccelerometer oGyro oNorth finder_oINS&IMU SINCE2008 • Inertial Attitude Measurement Manufacturer

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RION/MEMS IMU with GPS output pitch roll heading acceleration and angular speed/IMU560 - 13

IMU560 COMBINED INERTIAL NAVIGATION 3.1.1 Attitude output IMU_OUT_EULER Attitude angle includes Roll, Pitch and Yaw, use real32(float) to indicate, 12 bytes, unit is radians. Store format: Roll Pitch Yaw 3.1.2 Sensor output after calibration IMU_OUTPUT_GYROSCOPES 3 axis gyro angular rate after calibration Gx, Gy and Gz, use real32(float) to indicate, 12 bytes, unit is rad.S-1(radian/second). Store format: Gx Gy Gz IMU_OUTPUT_ACCELEROMETERS 3 axis acceleration after calibration Ax, Ay and Az, use real32(float) to indicate, 12 bytes, unit is m.S-20 Store format: Gx Gy Gz...

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