Website:
SHENZHEN RION TECHNOLOGY CO.,LTD
RION/dynamic tilt sensor inclination angle sensor anti-vibration inclinometer digital output/HDA436T
24Pages
Catalog excerpts
HDA436T HIGH-PRECISION DYNAMIC TILT SENSOR HIGH-PRECISION DYNAMIC TILT SENSOR ○Tilt sensor ○Electric Compass ○Digital Inclinometer ○Accelerometer ○Gyro ○North Finder ○INS&IMU SINCE2008 · Expert Of Inertial Attitude Measurement
Open the catalog to page 1
HDA436T HIGH-PRECISION DYNAMIC TILT SENSOR PRODUCTION EXECUTION STANDARD REFERENCE ○ Enterprise quality system standard: ISO9001: 2015 standard (certification number: 128101)； ○ The intellectual property management system complies with the standard: GB / T 29490-2013 (Certificate No.: 18117IP1529R0S)； ○ High-tech enterprise (Certificate No .: GR201844204379)； ○ Angle sensor production standard: SJ20873-2003 General specification for inclinometer and spirit level ○ Gyro acceleration test standard: QJ 2318-92 gyro accelerometer test method； ○ Software development reference standard: GJB...
Open the catalog to page 2
HDA436T HIGH-PRECISION DYNAMIC TILT SENSOR ▶ PRODUCT DESCRIPTION HDA436T，A new generation of digital MEMS dynamic tilt sensor launched by RION Technology. It can measure the attitude parameters (roll, pitch, and azimuth) of a moving carrier, and suitable for tilt angle measurement under motion or vibration. HDA436T has a built-in high-precision acceleration and gyro sensor, and integrates the Carman filter algorithm, which can measure the real-time motion data of the carrier under motion or vibration. The signal output modes such as RS485 / 232 / TTL are optional, and the scalability is...
Open the catalog to page 3
HDA436T HIGH-PRECISION DYNAMIC TILT SENSOR ► TECHNICAL PARAMETERS Resolution : It refers to the smallest change in the measured value that can be detected and resolved by the sensor within the measurement range. Absolute accuracy : Absolute accuracy refers to the comprehensive error of the sensor's absolute linearity, repeatability, hysteresis, zero point deviation, and horizontal axis error under normal temperature conditions. Response time : The response time is the time required for the sensor output to reach the measured value when the sensor changes its angle once. oTilt...
Open the catalog to page 4
HDA436T HIGH-PRECISION DYNAMIC TILT SENSOR Output Interface Installation Direction BIN: Binary protocol MB: MODBUS protocol VR: vertical Right E.g: HDA436T-485-BIN: horizontal installation / BIN: Binary protocol. ▶ MECHANICAL PARAMETERS ○ Connector: M12 aviation plug 5P connector ○ Protection level: IP67 ○ Shell material: frosted aluminum alloy ○ Installation: Four M4 screws WORKING PRINCIPLE Adopt imported core control unit and apply the principle of capacitive miniature pendulum. Using the earth's gravity principle, when the tilt unit tilts, the earth's gravity will produce a...
Open the catalog to page 5
HDA436T HIGH-PRECISION DYNAMIC TILT SENSOR ▶ PRODUCT SIZE CHART ▶ ELECTRICAL CONNECTIONS RS485 WIRING DEFINITION PIN FUNCTION ○Tilt sensor ○Electric Compass ○Digital Inclinometer ○Accelerometer ○Gyro ○North Finder ○INS&IMU SINCE2008 · Expert Of Inertial Atti
Open the catalog to page 6
HDA436T HIGH-PRECISION DYNAMIC TILT SENSOR ▶ INSTALLATION METHOD ○Tilt sensor ○Electric Compass ○Digital Inclinometer ○Accelerometer ○Gyro ○North Finder ○INS&IMU SINCE2008 · Expert Of Inertial Attitu
Open the catalog to page 7
► BINARY PROTOCOL COMMUNICATION PROTOCOL 1.0 Communication Frame Format Notes: A. The data length field includes the number of data fields (Datas). MSB comes first, LSB comes after. A length of 0 indicates no data field. The longest data field is 504 bytes, and the longest frame byte is 512. Bytes. B. The calculation of CRC starts from ADDR, including CMD, length field and data field, MSB first, LSB last, and calculate CRC according to the following function: uintl6 calcCRC(const uint8 *pBuffer, uintl6 bufferSize) { ' uintl6 poly = 0x8408; uintl6 crc = 0; uint8 carry; uint8 i_bits; uintl6...
Open the catalog to page 8
2.1.1 Response The response frame format is as follows: The order indicates the order of data output. 3.2 Data Output Format 3.2.1 Attitude angles Roll, Pitch and Yaw, expressed in real32 (float), 12 bytes, in radians. Storage format: Roll Pitch Yaw 3.2.2 Three-Axis Gyro Angular Rate Gx, Gy And Gz, Expressed In Real32 (Float), 12 Bytes, The Unit Is Rad.S-1 (Radian / Second). Storage format: Gx Gy Gz 3.2.3Three-Axis Acceleration Ax, Ay And Az, Expressed In Real32 (Float), 12 Bytes, The Unit Is m.S-20 Storage format: Ax Ay Az oTilt sensor_oElectric Compass_oDigital...
Open the catalog to page 9
3.3 Output Data Order According to different values of output masks (uint32), the corresponding output order will be generated. The default output masks (uint32) = 0x00000007 is as follows: IMU_OUTPUT_EULER | IMU_OUTPUT_GYROSCOPES | IMU_OUTPUT_ACCELEROMETERS (0x00000001 | 0x00000002 | 0x00000004) The corresponding output data sequence and storage format are as follows: oTilt sensor_oElectric Compass_oDigital Inclinometer_oAccelerometer_oGyro_oNorth Finder_oINS&IMU SINCE2008 ■ Expert Of Inertial Attitude Measurement
Open the catalog to page 10
4. 2 Get Data Items For Automatic Output * IMU_GET_DEFAULT_OUTPUT_MASK------(0x51) Function: It is used to read the output MASK (output mask (uint32)) data item, which is used for data analysis. The frame format is as follows: Number Field oTilt sensor_oElectric Compass_oDigital Inclinometer_oAccelerometer_oGyro_oNorth Finder_oINS&IMU SINCE2008 ■ Expert Of Inertial Attitude Measurement
Open the catalog to page 11
SINCE2008 ■ Expert Of Inertial Attitude Measurement
Open the catalog to page 12
Function: used to read the current mode; The frame format is as follows: oTilt sensor_oElectric Compass_oDigital Inclinometer_oAccelerometer_oGyro_oNorth Finder_oINS&IMU SINCE2008 ■ Expert Of Inertial Attitude Measurement
Open the catalog to page 13
Function: Used to get the communication baud rate; The frame format is as follows: oTilt sensor_oElectric Compass_oDigital Inclinometer_oAccelerometer_oGyro_oNorth Finder_oINS&IMU SINCE2008 ■ Expert Of Inertial Attitude Measurement
Open the catalog to page 14
Function: return the sensor address; The frame format is as follows: Of which: DATA part oTilt sensor_oElectric Compass_oDigital Inclinometer_oAccelerometer_oGyro_oNorth Finder_oINS&IMU SINCE2008 ■ Expert Of Inertial Attitude Measurement
Open the catalog to page 15
Fixed_Mode 1 4.13 Set Gravity Magnitude * IMU_SET_GRAVITY_MAGNITUDE------(0xB1) Function : set current gravity magnitude level ; Note: It does not have the power-down save function. You must execute the save setting command to save The frame format is as follows: Of which: DATA part oTilt sensor_oElectric Compass_oDigital Inclinometer_oAccelerometer_oGyro_oNorth Finder_oINS&IMU SINCE2008 ■ Expert Of Inertial Attitude Measurement
Open the catalog to page 16All SHENZHEN RION TECHNOLOGY CO. catalogs and technical brochures
-
accelerometer for wind power37 Pages
-
3 AXIS ATTITUDE GYRO RION TL735G18 Pages
-
AH200C MEMS18 Pages
-
RION ACA2000T11 Pages
-
Rion Product Catalog23 Pages
-
TL766D Azimuth Angle Sensor8 Pages
-
3R30-05 3Axis Turntable4 Pages
-
NF601North finder13 Pages
