Aerodynamic parameter estimation of an Unmanned Aerial Vehicle based on extended kalman filter and its higher order approach

Aerodynamic parameter estimation provides an effective way for aerospace system modelling using measured data from flight test, especially for the purpose of developing elaborate simulation environments and control systems design of Unmanned Aerial Vehicle (UAV) with short design cycles and reduced...

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Vydané v:	2010 2nd International Conference on Advanced Computer Control Ročník 5; s. 526 - 531
Hlavní autori:	Li Meng, Liu Li, Veres, S M
Médium:	Konferenčný príspevok..
Jazyk:	English
Vydavateľské údaje:	IEEE 01.03.2010
Predmet:	Aerodynamic Parameter Estimation Aerodynamics Aerospace control Aerospace simulation Aerospace testing Extended Kalman Filter (EKF) Filtering Nonlinear dynamical systems Parameter estimation System testing Unmannd Aerial Vehicle (UAV) Unmanned aerial vehicles Vehicle dynamics
ISBN:	1424458455, 9781424458455
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