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Flight Dynamics and System Identification for Modern Feedback Control
book

Flight Dynamics and System Identification for Modern Feedback Control

by J Grauer, J Hubbard Jr.
October 2013
Intermediate to advanced
160 pages
3h 48m
English
Woodhead Publishing
Content preview from Flight Dynamics and System Identification for Modern Feedback Control

Appendix A: Field calibration of inertial measurement units

Abstract: Inertial measurement units (IMUs) consist of orthogonal triads of magnetometers, gyroscopes, and accelerometers, and are used in autopilots to provide information on the vehicle pose and motion. The IMUs used on unmanned aircraft suffer from the low signal-to-noise ratios and strong temperature dependencies typical of Microelectromechcanical systems (MEMS) devices, requiring tedious laboratory testing or on-board state estimators for calibration. In this appendix, a method is presented for estimating IMU calibration constants, based on three successive least-squares computations. Memory and computation requirements are low enough for implementation on 8 bit microprocessors, ...

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Publisher Resources

ISBN: 9780857094667