A simple testing device is presented that simultaneously calibrates all dominant error sources for accelerometers and gyroscopes found in typical microelectromechanical inertial measurement units on smart projectiles, including bias, scale factor, cross axis sensitivity/misalignment, and misposition. The device consists of a table which rotates about a gimbal joint and is supported on the corners by elastic and damping elements. Using dynamic simulation it is shown that motion created by free vibration of the testing platform suitably excites sensors on projectiles so calibration can be performed. Calibration parameters are estimated using an extended Kalman filter. Platform support stiffness and damping characteristics significantly alter the time required to identify calibration parameters by shaping platform motion. A critical level of initial motion of the testing platform is required for adequate prediction of calibration parameters.
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Production Line Calibration for Sensors on Actively Controlled Bullets
Mark Erickson, Graduate Research Assistant,
Mark Erickson, Graduate Research Assistant
Department of Mechanical Engineering, Oregon State University, Corvallis, OR 97331
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Mark Costello, Assistant Professor
Mark Costello, Assistant Professor
Department of Mechanical Engineering, Oregon State University, Corvallis, OR 97331
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Mark Erickson, Graduate Research Assistant
Department of Mechanical Engineering, Oregon State University, Corvallis, OR 97331
Mark Costello, Assistant Professor
Department of Mechanical Engineering, Oregon State University, Corvallis, OR 97331
Contributed by the Manufacturing Engineering Division for publication in the JOURNAL OF MANUFACTURING SCIENCE AND ENGINEERING. Manuscript received May 2002; Revised December 2003. Associate Editor: K. Danai.
J. Manuf. Sci. Eng. May 2004, 126(2): 368-376 (9 pages)
Published Online: July 8, 2004
Article history
Received:
May 1, 2002
Revised:
December 1, 2003
Online:
July 8, 2004
Citation
Erickson, M., and Costello, M. (July 8, 2004). "Production Line Calibration for Sensors on Actively Controlled Bullets ." ASME. J. Manuf. Sci. Eng. May 2004; 126(2): 368–376. https://doi.org/10.1115/1.1688376
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