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contributor authorMark Erickson
contributor authorGraduate Research Assistant
contributor authorMark Costello
date accessioned2017-05-09T00:13:40Z
date available2017-05-09T00:13:40Z
date copyrightMay, 2004
date issued2004
identifier issn1087-1357
identifier otherJMSEFK-27811#368_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/130407
description abstractA 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.
publisherThe American Society of Mechanical Engineers (ASME)
titleProduction Line Calibration for Sensors on Actively Controlled Bullets
typeJournal Paper
journal volume126
journal issue2
journal titleJournal of Manufacturing Science and Engineering
identifier doi10.1115/1.1688376
journal fristpage368
journal lastpage376
identifier eissn1528-8935
keywordsAccelerometers
keywordsCalibration
keywordsErrors
keywordsSensors
keywordsProjectiles
keywordsBullets
keywordsKalman filters AND Motion
treeJournal of Manufacturing Science and Engineering:;2004:;volume( 126 ):;issue: 002
contenttypeFulltext


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