A Complementary filter for attitude Estimation of a fixed-Wing UAV
This paper considers the question of using a nonlinear complementary filter for attitude estimation of fixed-wing unmanned aerial vehicle (UAV) given only measurements from a low-cost inertial measurement unit. A nonlinear complementary filter is proposed that combines accelerometer output for low frequency attitude estimation with integrated gyrometer output for high frequency estimation. The raw accelerometer output includes a component corresponding to airframe acceleration, occurring...[Show more]
|Collections||ANU Research Publications|
|Source:||Proceedings of IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS 2008)|
|01_Euston_A_Complementary_filter_for_2008.pdf||602.51 kB||Adobe PDF||Request a copy|
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