BW-IMU200 Serials. Low-cost Inertial Measurement Unit. Technical Manual

Similar documents
BW-VG525 Serials. High Precision CAN bus Dynamic Inclination Sensor. Technical Manual

IMU60 Inertial Measurement Unit

SPECIFICATIONS. ACA2000 -High Accuracy Digital Type Dual-Axis Inclinometer with Full Temperature Compensation. Item No.:ACA2000

MGA103 Single Axis MEMS Gyro with Triaxial Accelerometer

MG100 Single Axis MEMS Gyro

OS3D-FG MINIATURE ATTITUDE & HEADING REFERENCE SYSTEM MINIATURE 3D ORIENTATION SENSOR OS3D-P. Datasheet Rev OS3D-FG Datasheet rev. 2.

3DM-GX4-45 LORD DATASHEET. GPS-Aided Inertial Navigation System (GPS/INS) Product Highlights. Features and Benefits. Applications

3DM -CV5-10 LORD DATASHEET. Inertial Measurement Unit (IMU) Product Highlights. Features and Benefits. Applications. Best in Class Performance

TL632D- MEMS Digital Type Gyroscope SPECIFICATIONS. Item No.:TL632D. Description:MEMS Digital Type Gyroscope. Version:Ver.05

SPECIFICATIONS. DCM302B-High Accuracy 3D Electronic Compass(2D Calibration) Item No.:DCM302B

INERTIAL LABS SUBMINIATURE 3D ORIENTATION SENSOR OS3DM

An internal gyroscope minimizes the influence of dynamic linear acceleration on slope sensor readings.

CMPS11 - Tilt Compensated Compass Module

Features. Description. General Specifications. VS Series Inclinometer : Dual Axis, RS232 and Analogue Output

High Performance Advanced MEMS Industrial & Tactical Grade Inertial Measurement Units

Parameter Value Unit Notes

SOLAR-360 : 360 Inclinometer, RS232 or RS485 Output

CMPS09 - Tilt Compensated Compass Module

Picture 1 PC & USB Connection

P/N: AX06080X. TECHNICAL DATASHEET #TDAX06080X Triaxial Inclinometer SAE J1939 or CANopen 2 M12 Connector(s), IP67 with Electronic Assistant

SOLAR-2 : Dual Axis Inclinometer, RS232 or RS485 Output

Attitude and Heading Reference Systems

FLCS V2.1. AHRS, Autopilot, Gyro Stabilized Gimbals Control, Ground Control Station

Date: January 16, 2003 Page 1 of 1

IMU Platform for Workshops

AHRS400 Series User s Manual

ASC IMU 7.X.Y. Inertial Measurement Unit (IMU) Description.

INCLINOMETER RS232 SWITCH

ability design, selected proven components directory, finite element analysis (thermal reliability analysis,

Installation Instructions for the Transportation Attitude Reference System (TARS Series) Ruggedized Inertial Measurement Unit (IMU)

H3-IMU High Performance Inertial Measurement Unit

Model D875 Mini Tuff Tilt Digital Tiltmeter

GPS-Aided INS Datasheet Rev. 2.6

P2-AHU Manual v1.0. P2-AHU Manual. (T-Module) - 1 -

Inertial Sensors. Ellipse Series MINIATURE HIGH PERFORMANCE. Navigation, Motion & Heave Sensing IMU AHRS MRU INS VG

Data Sheet THE SCA121T DUAL AXIS INCLINOMETER MODULES. Features. Applications

Inertial Sensors. Ellipse 2 Series MINIATURE HIGH PERFORMANCE. Navigation, Motion & Heave Sensing IMU AHRS MRU INS VG

Inertial Sensors. Ellipse 2 Series MINIATURE HIGH PERFORMANCE. Navigation, Motion & Heave Sensing IMU AHRS MRU INS VG

GPS-Aided INS Datasheet Rev. 2.7

Technical Manual. CruizCore R1350N Rev Copyright Microinfinity Co., Ltd.

Inertial Sensors. Ellipse Series MINIATURE HIGH PERFORMANCE. Navigation, Motion & Heave Sensing IMU AHRS MRU INS VG

SSI Inclinometer. Zigbee. CDMA Vibration-wire. SSI PWM Switch Analog. Features. Descriptions

Motion Reference Units

X3M. Multi-Axis Absolute MEMS Inclinometer Page 1 of 13. Description. Software. Mechanical Drawing. Features

GPS-Aided INS Datasheet Rev. 2.3

GPS-Aided INS Datasheet Rev. 3.0

UNSTAR 传感与控制 TEL: FAX: szss AHRS300 Series User s Manual AHRS300CA- (DMU-AHRS) Revision 1.5

GPRS Inclinometer. Zigbee. CDMA Vibration-wire. SSI PWM Switch Analog. Features. Descriptions

TFmini Infrared Module Specification

Installation Instructions for the Transportation Attitude Reference Sensor TARS Series

TL618D- MEMS Current Type Gyroscope SPECIFICATIONS. Item No.:TL618D. Description:MEMS Current Type Gyroscope. Version:Ver.05

Dynamic Angle Estimation

ADMA. Automotive Dynamic Motion Analyzer with 1000 Hz. ADMA Applications. State of the art: ADMA GPS/Inertial System for vehicle dynamics testing

Motion Reference Units

HG1120 INERTIAL MEASUREMENT UNIT (IMU) Installation and Interface Manual

SKD-600D Laser Distance Sensor

USART Digital Compass Manual

TF02 Single-point Ranging LiDAR Product Specification

Specifications Attitude and Heading Specifications. GP9 GPS-Aided AHRS Datasheet, Revision 1.3

OughtToPilot. Project Report of Submission PC128 to 2008 Propeller Design Contest. Jason Edelberg

NRA24 millimeter wave radar User manual

SERIES VECTORNAV TACTICAL SERIES VN-110 IMU/AHRS VN-210 GNSS/INS VN-310 DUAL GNSS/INS

Mercury technical manual

SPECIFICATIONS. AKE390B-MEMS Voltage Type Accelerometer. Item No.:AKE390B. Description:MEMS Voltage Type Accelerometer. Version:Ver.

Communications message formats

MTi 100-series The most accurate and complete MEMS AHRS and GPS/INS

Accelerometer user manual

If you want to use an inertial measurement system...

SPECIFICATIONS. Item No.:AKE398B. Description:MEMS Current Type Accelerometer. Version:Ver.06. AKE398B-MEMS Current Type Accelerometer

Cost efficient design Operates in full sunlight Low power consumption Wide field of view Small footprint Simple serial connectivity Long Range

302 VIBROENGINEERING. JOURNAL OF VIBROENGINEERING. MARCH VOLUME 15, ISSUE 1. ISSN

HPC Compass NMEA Version. Installation and Operation Manual

Cost efficient design Operates in full sunlight Low power consumption Wide field of view Small footprint Simple serial connectivity Long Range

3DM-GX3-45 Theory of Operation

Application Note. Communication between arduino and IMU Software capturing the data

CENG 5931 HW 5 Mobile Robotics Due March 5. Sensors for Mobile Robots

Extended Kalman Filtering

SENLUTION Miniature Angular & Heading Reference System The World s Smallest Mini-AHRS

MTi 100-series The most accurate and complete MEMS AHRS and GPS/INS

User manual. Inclinometer with Analog-RS232-Interface IK360

USER GUIDE OCTANS III & POSITIONING NAVIGATION II. PART 2 : OCTANS III SURFACE USER GUIDE

Migrating from the 3DM-GX3 to the 3DM-GX4

OBSOLETE. Digital Output, High Precision Angular Rate Sensor ADIS Data Sheet FEATURES GENERAL DESCRIPTION APPLICATIONS FUNCTIONAL BLOCK DIAGRAM

SPEEDBOX Technical Datasheet

Orientus Reference Manual

HG G B. Gyroscope. Gyro for AGV. Device Description HG G B. Innovation through Guidance. Autonomous Vehicles

HG4930 INERTIAL MEASUREMENT UNIT (IMU) Performance and Environmental Information

GPS Time and Frequency Reference Receiver

Module 2: Lecture 4 Flight Control System

Reference Diagram IDG-300. Coriolis Sense. Low-Pass Sensor. Coriolis Sense. Demodulator Y-RATE OUT YAGC R LPY C LPy ±10% EEPROM TRIM.

Instruction Manual Single and Dual Axis Inclinometer P-Series

How to introduce LORD Sensing s newest inertial sensors into your application

K-Band Doppler Sensor Module

±300 /sec Yaw Rate Gyro ADXRS620

Device manual Inclination sensor 2 axes JN /00 04/2015

E31-TTL-500 Datasheet V Feature E31-TTL-500

Inertial Systems. Ekinox Series TACTICAL GRADE MEMS. Motion Sensing & Navigation IMU AHRS MRU INS VG

Integrated Dual-Axis Gyro IDG-1004

xoem500 Hardware Integration Manual Inertial and GNSS measurement system Confidently. Accurately.

Revisions Revision Date By Changes A 11 Feb 2013 MHA Initial release , Xsens Technologies B.V. All rights reserved. Information in this docum

Transcription:

Serials Low-cost Inertial Measurement Unit Technical Manual

Introduction As a low-cost inertial measurement sensor, the BW-IMU200 measures the attitude parameters of the motion carrier (roll angle, pitch angle, angular velocity, acceleration).attitude and angular velocity deviations are estimated by a 6-state Kalman filter with appropriate gain, that is suitable for inertial attitude measurement in motion or vibration. BW-IMU200 uses highly reliable MEMS accelerometers and gyroscopes,and ensure measurement accuracy through algorithms, meanwhile, the seal design and strict process ensure that the dynamic parameters of the carrier such as the angular velocity acceleration and attitude can be accurately measured under harsh conditions. Through various compensations such as nonlinear compensation, quadrature compensation, temperature compensation and drift compensation, the error source of BW-IMU200 can be greatly eliminated, and the product accuracy level can be improved. The BW-IMU200 is equipped with digital interface that can be easily integrated into the user's system. Features Dynamic compensation and quadrature compensation Accuracy:1 Special offset tracking algorithm eliminates drift Gyro drift compensation Standard RS232/RS485/TTL output interface Operating temperature:: -40 +85,temperature compensation High-performance Kalman filter algorithm Small size: L60 W59 H29mm Applications Ship Construction machinery Platform stability Agricultural machinery Special vehicle Driverless Robot Aircraft

Specifications Electrical Specifications Power supply Operating current Operating temperature Store temperature 9-35V DC 40mA (DC 12V ) -40~85-55~100 Performance Specifications Accuracy 1 Pitch angle Resolution 0.01 measuring range -90 ~90 Roll angle Gyro Accelerometer Maximum output frequency Start delay Anti-vibration performance Accuracy Resolution Range Resolution Range Zero instability ARW Noise density Zero absolute error Range: X,Y,Z Resolution Bias stability 100Hz 50ms 2000g 2 0.01-180 ~180 0.02 /sec ±500 /sec 50 /h 1.6 / h 0.005 /s/ Hz ±0.2 /sec ±2 g 1 mg ±4 mg

Resolution: The measured minimum change value that the sensor can detect and resolve within the measurement range. Accuracy: The error between the actual angle and the Root mean square(rms) of the measured angle of the sensor ( 16 times). Mechanical Characteristic Connector Protection level Shell material Installation Metal connector(standard cable is 1.5m)) IP67 Magnesium alloy sanding oxidation Four M4 screws Package size Product Size:L60*W59*H29(mm) Bare plate product size Product size:l44*w35*h11(mm) Note: ±1mm error for length and width dimensions, please refer to actual size 39 hole Φ 2mm 30 35 44

Installation direction The correct installation method can avoid measurement error. The following points should be made when installing the sensor: First of all, to ensure that the sensor mounting surface and the measured surface completely close, the measured surface should be as horizontal as possible, can not have the angle shown in Figure A and Figure C, the correct installation is shown in Figure B and Figure D. A B uneven surface generates the angle the measured surface the measured surface C D uneven surface generates the angle the measured surface the measured surface Secondly, the bottom cable of the sensor and the axis of the measured object shouldn't generate the angle shown in E. When installing, the bottom cable of the sensor should be kept parallel or orthogonal to the rotation axis of the measured object. This product can be installed horizontally or vertically (vertical installation requires customization). The correct installation method is shown in Figure F. Finally, the installation surface of the sensor must be fixed with the measured surface tightly and smoothly, to avoid measurement error that may be caused by the acceleration and vibration.

Electrical connections Electrical interfaces Cable color & function RED 1 VCC DC 9-35V BLUE 2 NC BLACK 3 GND GREEN 4 RXD (B D-) YELLOW 5 TXD (A D+) Inertial 1 measureme 7 3 nt unit Sensor 1 5 4 3 DC 10-35V YELLOW: TXD RED VCC DC 9-35V YELLOW A GREEN B BLACK GND 485+ 485- GND 6 acquisition 2 3 4 5 1 Signal terminal 8 9 RS 485 wiring diagram Inertial measureme nt unit 1 5 4 3 RED VCC YELLOW TXD GREEN RXD BLACK GND DC 9-35V 1 2 3 4 5 6 7 8 9 GND RS 232 wiring diagram Note: The RS232 interface needs to share the product ground wire with the communication ground wire.

Debugging software Users can directly download serial assistant on official website (Supports-Download). You can also use more convenient and intuitive PC software. BW-IMU200 supporting serial debugging software can be connected to the inclinometer on the computer for angle display. The software debugging interface is as shown in the figure below. Using the debug software, it can conveniently display the current X-direction tilt angle, and you can also modify and set other parameters by yourself. Software usage steps 1 2 3 Connect the serial port hardware of the inclinometer correctly and connect the power supply. Select the computer serial port and baud rate and click to connect to the serial port. Click Start and the tilt angle of the inclinometer in the X and Y directions will be displayed on the screen.

Protocol 1 Frame Format: (8 data bits,1 stop bit,no parity check,default baud rate 9600) (Xbyte) H Format: Hexadecimal : Fixed to 77 : Length from to (included) : Address of acquiring module, default 0x00 : Content and length variable according to : Sum of,, and. (Please pay attention that when the command or data changes, the checksum will change. ) 2 Format: 2.1 Read PITCH angle :77 04 00 01 05 0x01 response: (3byte) 0x07 0x81 SXXX.YY Note: represents 3 byte angle value in format of compressed BCD code. S is the sign bit (0 means positive, 1 means negative), XXX is the three digit integer part, YY is the fractional part. For example, if the return value is 77 07 00 81 10 34 63 2F, the pitch angle data is 10 34 63, which means -34.63 degrees. 2.2 Read ROLL angle : 77 04 00 02 06 0x02 0x06 response: (3byte) 0x07 0x82 SXXX.YY Note: represents 3 byte angle value in format of compressed BCD code. S is the sign bit (0 means positive, 1 means negative), XXX is the three digit integer part, YY is the fractional part.for example, if the return value is 77 07 00 82 01 23 57 04, the roll angle data is "01 23 57", which means "123.57 degrees"

2.3 Read PITCH, ROLL axis angle :77 04 00 04 08 response: (9byte) 0x0D 0x84 SXXX.YY PITCH axis: +2.01,ROLL axis: -0.51,YAW axis:0.00 77 0D 00 84 00 02 01 10 00 51 00 00 00 F5 ; fixed as 77 The length of the data, fixed to 0D means that in addition to 77, there are 13 bytes behind Address code, default is 00 word, fixed at 84 ROLL axis angle: The format is the same as the PITCH axis PITCH axis angle: The first digit of the first byte is the sign bit, 0 is the positive angle, and 1 is the negative angle. The second and second bytes of the first byte are integer bits of the angle, which are compressed BCD codes. The third byte is the decimal place of the angle, which is the compressed BCD code. YAW axis or reserved bit angle: the format is the same as the PITCH axis The last byte is the sum of all the previous data except the first number (). If there is a carry, the lower data is taken.

2.4 Set baud rate :77 05 00 0B 02 12 0x0B XX response: 0x8B 0x00: success 0xFF: failure Note: 0x00 means 2400 0x01 means 4800 0x02 means 9600 0x03 means 19200, means 115200, default value is 0x02:9600 Each time the communication baud rate is changed successfully, the response command is sent back at the original baud rate, and then the device communication baud rate is changed immediately. Note: If high frequency output is required, set the baud rate to 115200. Modify the baud rate without sending a save command, and it will take effect immediately. 2.5 Set module address :77 05 00 0F 01 15 correct address 0x0F new address response: new address 0x8F 0x00: success 0xFF: failure Note: For example, the following command "77 05 00 0F 0A 1E" means that the address of the product is changed from hexadecimal address 00 to 0A. 2.6 Query current address : 77 04 00 1F 23 0x00 0x1F 0x23 response: new address 0x1F new address Note: The query address command is to fix the command.

2.7 Set the output frequency :77 05 00 0C 00 11 0x0C XX response: 0x8C 0x00: success 0xFF: failure The transmitted data field XX is the automatic output frequency option: 00 indicates the answer mode, 01 indicates 5Hz automatic output corresponding data type parameter 02 indicates 10Hz automatic output corresponding data type parameter 03 indicates 20Hz automatic output corresponding data type parameter 04 indicates 25Hz automatic output corresponding data type parameter 05 indicates 50Hz automatic output corresponding data type parameter 06 indicates 100HZ automatic output Corresponding data type parameter Note: 1. When the automatic output frequency setting is high, the baud rate needs to be set to a high baud rate. Under some data types, 100HZ cannot be output due to the baud rate limit. 2. The automatic output data type parameter is determined according to the following data type selection command. The default is the automatic output angle. 2.8 Query gravitational acceleration g : 77 04 00 54 58 0x54 response: (9byte) 0x0D 0x54 SXYYYY Note: The data field part is the value of g value of pitch, roll, Z axis (vertical horizontal plane), which consists of 1 bit sign bit + 1 bit integer bit + 4 decimal places. If the return value is "77 0D 00 54 00 01 07 00 94 21 10 06 30 64", they are 0.0107g, 0.9421g, -0.0630g respectively.

2.9 Query angular velocity : 77 04 00 50 54 0x50 response: (9byte) 0x0D 0x50 SXXXYY Note: The data field is the pitch, roll, and Z-axis (vertical horizontal) angular velocity. It consists of 1 sign bit + 3 integer bits + 2 decimal places. For example, the return value is 77 0D 00 50 10 93 76 14 98 87 00 14 03 C0. The data field parts are: pitch axis angular velocity: -93.76 /s, roll axis angular velocity: -498.87 /s Z-axis angular velocity :+14.03 /s 2.10 Save settings : 77 04 00 0A 0E 0x0A response: 0x8A 00:success FF: failure Note: It is not necessary to save the settings to set the baud rate. Other settings need to send the save settings. 2.11 Quaternion : 77 04 00 57 5B 0x57 response: (16byte) 0x14 0x57 SXYYYYYY Note: The data field contains 16 bytes, 4 bytes are a group, respectively quaternary q0, q1, q2, q3, which is a compressed BCD code, the format is SX YY YY YY, S is a sign bit (0 positive, 1 negative), X is a 1-bit integer bit, and YYYYYY is a 6-digit decimal place. For example, the return command 77 14 00 57 00 99 99 96 00 00 02 90 10 00 26 73 10 00 00 01 7F Then the quaternion data are: Where q0 is 00 99 99 96, representing 0.999996. q1 is 00 00 02 90, which means 0.000290 q2 is 10 00 26 73, which means -0.002673 q3 is 10 00 00 01, indicating -0.000001

2.12 Simultaneous reading angle, accelerometer, gyroscope, quaternion : 77 04 00 59 5D 0x59 - response: (43byte) 0x2F 0x59 field Note: The data field contains 43 bytes, which are angle, gravitational acceleration g value, angular velocity, quaternion, compressed BCD code, four elements are the last 16 bytes, 4 bytes are a group, a total of 4 groups The rest is a group of 3 bytes, indicating the method to see the corresponding parameter return value. For example, the return value is: 77 2F 00 59 10 00 60 10 03 06 00 00 00 10 01 07 10 05 43 01 01 54 10 00 13 10 00 04 00 00 09 10 87 06 35 00 01 76 91 00 02 06 94 00 49 11 75 5C Then: the three axis angles are -0.6 degrees, -3.06 degrees, 0 degrees; The g values of the three axes were -0.0107 g, -0.0543 g, and 1.0154 g, respectively; The three angular angular velocities are -0.13 / s, -0.04 / s, 0.09 / s; The four quaternions are -0.870635, 0.017691, 0.020694, 0.491175 2.13 Automatic output data type selection : 77 05 00 56 00 5B 0x56 XX response: 0x56 00 Note: field XX is the corresponding output data type, which needs to be performed in automatic output mode: 0x00: When outputting automatically, the output parameter is triaxial angle data, and the output format refers to command 2.3; 0x01: When the output is automatic, the output parameter is the triaxial acceleration value, and the output format refers to the command 2.8; 0x02: When outputting automatically, the output parameter is the value of the three-axis gyroscope, and the output format refers to the command 2.9; 0x03: When outputting automatically, the output parameter is triaxial angle data (reserving other data types); : When outputting automatically, the output parameter is a quaternion value, and the output format refers to the command 2.11. : When outputting automatically, the output parameters are composed of angle, acceleration, angular velocity and four elements. The output format refers to command 2.12.

Ordering Information Product number BW-IMU200-485 BW-IMU200-232 BW-IMU200-TTL Way of communication RS 485 RS232 TTL Package condition IP67 Package/Metal Connector IP67 Package/Metal Connector IP67 Package/Metal Connector Executive standard Enterprise Quality System Standard: ISO9001:2008 Standard (Certificate No.:10114Q16846ROS) CE certification (certificate number: 3854210814) ROHS (certificate number: SO81426003) GB/T 191 SJ 20873-2003 General specifications for tiltmeters and spirit levels GBT 18459-2001 sensor main static performance index calculation method JF 1059-1999 Evaluation and Expression of Measurement Uncertainty GBT 14412-2005 mechanical vibration and shock mechanical installation of accelerometer General requirements for GJB 450A-2004 equipment reliability Quality control of key parts and important parts of GJB 909A GJB 899 Reliability Qualification and Acceptance Test GJB 150-3A high temperature test GJB 150-4A low temperature test GJB 150-8A rain test GJB 150-12A dust test GJB 150-16A vibration test GJB 150-18A impact test GJB 150-23A Tilt and Swing Test GB/T 17626-3A RF electromagnetic radiation immunity test GB/T 17626-5A surge (hit) impulse immunity test GB/T 17626-8A power frequency magnetic field immunity test GB/T 17626-11A voltage dips, short interruptions and voltage changes immunity

Serials Low-cost inertial measurement unit Wuxi Bewis Sensing Technology LLC Address: Building 30, No. 58 Xiuxi Road, Binhu District, Wuxi City Hotline: 400-618-0510 Tel: +86 510 85737158 Email: sales@bwsensing.com Website: www.bwsensing.com