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29 

Document MT1600P.2019.A 

© Xsens Technologies B.V.

 

MTi Family Reference Manual 

 

Installation tips and tricks

 

6.1  Transient accelerations 

The 3D linear accelerometers in the MTi are primarily used to estimate the direction of gravity to obtain 

a reference for attitude (pitch/roll). During long periods (more than tens of seconds) of transient “free” 

accelerations  (i.e.  2

nd

  derivative  of  position)  the  observation  of  gravity  cannot  be  made.  The  sensor 

fusion  algorithms  can  mitigate  these  effects  to  a  certain  extent,  but  nonetheless  it  is  impossible  to 
estimate true vertical without additional information. 
 
The impact of transient accelerations can be minimized when you take into account a few things when 
positioning the device when installing it in the object you want to track/navigate/stabilize or control. 
 
If  you  want  to  use  the  MTi  to  measure  the  dynamics  of  a  moving  vehicle  it  is  best  to  position  the 
measurement device at a position close to the centre of rotation (CR) of the vehicle/craft. Any rotations 
around the centre of rotation translate into centripetal accelerations at any point outside the centre of 
rotation. For a GNSS/INS device with a valid GNSS-fix, the detrimental effect of transient accelerations 
on orientation estimates is overcome by integrating GNSS measurements in the sensor fusion engine.   
 

6.2  Vibrations 

The  MTi  samples  IMU  signals  at  high  frequency  per  channel,  processing  them  using  a  strapdown 
integration algorithm with coning/sculling compensation. Proper coning/sculling compensation already 
mitigates errors that poorly designed signal processing pipelines introduce when the device is under 
vibration.  For  best  results  however,  it  is  recommended  that  the  MTi  be  mechanically  isolated  from 
vibrations  as  much  as  possible:  since  vibrations  are  measured  directly  by  the  accelerometers,  the 
following two conditions can make the readings from the accelerometers invalid; 

1.  The magnitude of the vibration is larger than the measurement range of the accelerometer. This 

will cause the accelerometer to saturate, which may be observed as a “drift” in the zero

-level of 

the accelerometer. This will show up as an erroneous roll/pitch. 

2.  The frequency of the vibration is higher than the bandwidth of the accelerometer. In theory, such 

vibrations are rejected, but in practice they can still give rise to aliasing, especially if close to the 
bandwidth limit. This can be observed as a low frequency oscillation. Further, high frequency 
vibrations often tend to have large acceleration amplitudes (see item 1).  

 
There is an effect on the gyroscopes as well and especially when the vibrations include high-frequent 
coning motion, the gyroscope readings may become invalid.  
 

6.3  Magnetic materials and magnets 

When  an  MTi  is  placed  close  to  or  on  an  object  that  is  either  magnetic  or  contains  ferromagnetic 
materials,  the  measured  magnetic  field  is  distorted  (warped)  and  causes  an  error  in  the  computed 
heading.  The  earth  magnetic  field  is  altered  by  the  presence  of  ferromagnetic  materials,  permanent 
magnets or power lines with strong currents (several amperes) in the vicinity of the device. The distance 
to  the  object  and  the  amount  of  ferromagnetic  material  determines  the  magnitude  of  disturbance 
introduced. Errors in estimated yaw due to such distortions can be quite large, since the earth magnetic 
field is very weak in comparison to the magnitude of the sources of distortion. 
 
By default, the AHRS and the GNSS/INS versions (when using the GeneralMag filter profile) stabilize 
heading using the local Earth's magnetic field. In other words, the measured magnetic field is used as 
a compass. In addition, the gyroscope biases are continuously estimated by the MTi's on-board filter. 
For the rate of turn around the x-axis and the y-axis (roll and pitch axes), the gyroscope bias is estimated 

Содержание MTi Series

Страница 1: ...67 00 fax 31 0 88 973 67 01 e mail info xsens com internet www xsens com 101 N Pacific Coast Hwy Suite 101 El Segundo CA 90245 USA phone 310 481 1800 fax 310 416 9044 e mail info xsens com internet w...

Страница 2: ...rights reserved Information in this document is subject to change without notice Xsens MVN MotionGrid MTi MTx and Awinda are registered trademarks or trademarks of Xsens Technologies B V and or its p...

Страница 3: ...2 2 Orientation increment and Velocity increment dq and dv 16 4 2 3 Orientation data 17 4 2 4 Velocity data 18 4 2 5 Position data 19 4 3 PHYSICAL SENSOR MODEL 19 4 3 1 Calibrated q and v outputs 20 4...

Страница 4: ...A Xsens Technologies B V MTi Family Reference Manual 6 INSTALLATION TIPS AND TRICKS 29 6 1 TRANSIENT ACCELERATIONS 29 6 2 VIBRATIONS 29 6 3 MAGNETIC MATERIALS AND MAGNETS 29 7 WARRANTY AND LIABILITY 3...

Страница 5: ...onents of Development Kit 11 Table 4 Description of software components of Development Kit 12 Table 5 Conditions for the use of the MT Software Suite 13 Table 6 Data outputs with reference coordinate...

Страница 6: ...s for the use of Xsens products and inside information about installation MEMS sensors and GNSS receivers hardware design CAD files system architecture low level communication and sensor fusion algori...

Страница 7: ...Surface Mount Devices SMD module The MTi 600 series is a cost effective product line for easy integration The MTi 10 series2 is Xsens entry level model with robust accuracy The MTi 100 series is a Xse...

Страница 8: ...rence for roll and pitch calculations Essentially it delivers the same data as the AHRS except for the yaw The yaw estimate of a VRU product is unreferenced which means that it is computed without any...

Страница 9: ...e information 2 2 3 MTi 10 series The MTi 10 series offers inertial and orientation data at an affordable price It features a sturdy anodized aluminium housing and robust push pull connectors The MTi...

Страница 10: ...MTi 1 IMU MTi 610 IMU MTi 10 IMU MTi 100 IMU VRU MTi 2 VRU MTi 620 VRU MTi 20 VRU MTi 200 VRU AHRS MTi 3 AHRS MTi 630 AHRS MTi 30 AHRS MTi 300 AHRS GNSS INS MTi 7 GNSS INS MTi 670 GNSS INS MTi G 710...

Страница 11: ...Development Kit Depending on the model of MTi you have purchased the Development Kit can contain any of the following items Table 3 Description of hardware components of Development Kit Component Desc...

Страница 12: ...to online manuals Xsens Device API library MFM SDK Library Library for the Magnetic Field Mapper 3 1 1 Getting Started with MT Manager software The easiest way to get started with your MTi is to use M...

Страница 13: ...edded computers and microcontrollers The low level communication is extensively described in the MT Low Level Communication Protocol Documentation3 Next to that source code is delivered to make driver...

Страница 14: ...Not allowed to reverse engineer Allowed to execute reproduce modify and compile modified source code to use with Xsens products only Not allowed to modify DLL Include License Agreement with distribut...

Страница 15: ...tings Modelling Parameters Next to the calibration values shown in MT Manager each device is calibrated according to more complicated models to ensure accuracy e g non linear temperature effect cross...

Страница 16: ...Velocity increment Sensor fixed frame Sxyz or Oxyz Orientation increment Sensor fixed frame Sxyz or Oxyz Free acceleration Local earth fixed frame LXYZ default ENU Orientation Local earth fixed frame...

Страница 17: ...gles6 roll pitch yaw XYZ Earth fixed type are output following the aerospace sequence Z Y X Rotation Matrix directional cosine matrix A positive rotation is always right handed i e defined according t...

Страница 18: ...o mounting of the MTi on the automotive platform vehicle It is recommended to always mount the MTi with the x axis pointing to the front of the vehicle irrespective of the local coordinate frame used...

Страница 19: ...ata is used to relate the sampled digital voltages u from the sensors to the respective physical quantity s The gain matrix is split into a misalignment matrix A and a gain matrix G The misalignment s...

Страница 20: ...etic field data is in sensor fixed coordinate system Sxyz or Oxyz The units of the calibrated data output are as shown in Table 9 Table 9 Output specifications inertial and magnetometer data outputs V...

Страница 21: ...019 A Xsens Technologies B V MTi Family Reference Manual 4 3 4 Free acceleration Free acceleration Data ID 0x4030 is the acceleration in the local frame LXYZ from which the local gravity is deducted T...

Страница 22: ...re are several ways to mitigate the drift in yaw rotation around the z axis 1 When the MTi has sufficient movement in roll and pitch 30 degrees for more than 10 seconds the gyroscope bias will be esti...

Страница 23: ...c disturbances refer to chapter 6 3 of this document Next to the solutions described on the article Estimating Yaw in magnetically disturbed environments to mitigate effects from magnetic disturbances...

Страница 24: ...e optimized for different types of movement For optimal performance in a given application the correct filter profile must be set by the user Each product offer different filter profile options refer...

Страница 25: ...e Xsens filter output Currently only the Portable default and Airborne 4g platforms are supported The platform model can be configured using MT Manager or low level communication For more details on G...

Страница 26: ...erfaces for each product are available in the respective datasheets or hardware integration manuals Table 12 overview of interface options in MTi portfolio Interface MTi 1 series MTi 600 series I C SP...

Страница 27: ...MEA protocol As almost all GNSS receivers support the output of NMEA messages this functionality enables the use of virtually any GNSS receiver It is important to note that when using the NMEAin both...

Страница 28: ...the filter and user inputs Information contained within the status word are for example Selftest Filter valid GNSS fix No rotation update status Representative motion Clip flags of all axis gyroscopes...

Страница 29: ...the accelerometers the following two conditions can make the readings from the accelerometers invalid 1 The magnitude of the vibration is larger than the measurement range of the accelerometer This w...

Страница 30: ...incorrectly assuming that the device has rotated However in case of continuous magnetic disturbances 10 to 30 s depending on the filter settings the computed heading will slowly converge to a new sol...

Страница 31: ...current specifications for the Product for a period of one year from the date of delivery ANY LIABILITY OF XSENS WITH RESPECT TO THE SYSTEM OR THE PERFORMANCE THEREOF UNDER ANY WARRANTY NEGLIGENCE ST...

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