Dynamics modeling is becoming more and more important in the development and control of unmanned aerial vehicles (UAV). An accurate model of a vehicle requires good knowledge of the dynamics properties and motion states, which are usually estimated with the help of integrated inertial measurement units (IMUs). This work develops a special six degrees of freedom IMU, which has the capability of measuring the angular accelerations. This paper introduces the design of the new IMU along with its sensor models and calibration procedures. The work introduces two experimental methods to verify the calibrated IMU readings. The IMU was designed to support an on-line methodology to estimate the parameters of UAV’s dynamics model that is currently being developed by the authors.
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January 2013
Research-Article
Development of a Special Inertial Measurement Unit for UAV Applications
Khaled S. Hatamleh,
Khaled S. Hatamleh
Mechanical Engineering Department,
P.O. Box 3030,
Mechanical and Aerospace Engineering Department,
Las Cruces, NM 88003
e-mail: kshh@just.edu.jo; kshh@nmsu.edu
Jordan University of Science and Technology
,P.O. Box 3030,
Irbed 22110
, Jordan
;Mechanical and Aerospace Engineering Department,
New Mexico State University
,1040 S. Horseshoe Drive
,Las Cruces, NM 88003
e-mail: kshh@just.edu.jo; kshh@nmsu.edu
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Angel Flores-Abad,
Angel Flores-Abad
Graduate Student
e-mail: af_abad@nmsu.edu
Search for other works by this author on:
Pu Xie
Pu Xie
Graduate Student
e-mail: jackyxie@nmsu.edu
Mechanical and Aerospace Engineering Department,
1040 S. Horseshoe Drive,
Mechanical and Aerospace Engineering Department,
New Mexico State University
,1040 S. Horseshoe Drive,
Las Cruces, NM 88003
Search for other works by this author on:
Khaled S. Hatamleh
Mechanical Engineering Department,
P.O. Box 3030,
Mechanical and Aerospace Engineering Department,
Las Cruces, NM 88003
e-mail: kshh@just.edu.jo; kshh@nmsu.edu
Jordan University of Science and Technology
,P.O. Box 3030,
Irbed 22110
, Jordan
;Mechanical and Aerospace Engineering Department,
New Mexico State University
,1040 S. Horseshoe Drive
,Las Cruces, NM 88003
e-mail: kshh@just.edu.jo; kshh@nmsu.edu
Ou Ma
Professor
e-mail: oma@nmsu.edu
Angel Flores-Abad
Graduate Student
e-mail: af_abad@nmsu.edu
Pu Xie
Graduate Student
e-mail: jackyxie@nmsu.edu
Mechanical and Aerospace Engineering Department,
1040 S. Horseshoe Drive,
Mechanical and Aerospace Engineering Department,
New Mexico State University
,1040 S. Horseshoe Drive,
Las Cruces, NM 88003
Contributed by the Dynamic Systems Division of ASME for publication in the Journal of Dynamic Systems, Measurement, and Control. Manuscript received October 23, 2010; final manuscript received April 29, 2012; published online October 30, 2012. Assoc. Editor: Eugenio Schuster.
J. Dyn. Sys., Meas., Control. Jan 2013, 135(1): 011003 (10 pages)
Published Online: October 30, 2012
Article history
Received:
October 23, 2010
Revision Received:
April 29, 2012
Accepted:
May 7, 2012
Citation
Hatamleh, K. S., Ma, O., Flores-Abad, A., and Xie, P. (October 30, 2012). "Development of a Special Inertial Measurement Unit for UAV Applications." ASME. J. Dyn. Sys., Meas., Control. January 2013; 135(1): 011003. https://doi.org/10.1115/1.4007122
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