A non-linear observer for attitude estimation of a fixed-wing unmanned aerial vehicle without GPS measurements
In this paper we propose a simple non-linear observer for attitude estimation based only on output from a typical inertial measurement unit (IMU) and dynamic pressure sensor embarked on a low-cost unmanned aerial vehicle. In particular, we aim to provide
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|Source:||Transactions of the Institute of Measurement and Control|
|01_Mahony_A_non-linear_observer_for_2010.pdf||685.19 kB||Adobe PDF||Request a copy|
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