Aerodynamic Derivatives Identification Using a Non-Conservative Robust Kalman Filter
نویسندگان
چکیده
منابع مشابه
Aerodynamic parameter estimation using adaptive unscented Kalman filter
Purpose – The purpose of this paper is to estimate aerodynamic parameters accurately from flight data in the presence of unknown noise characteristics. Design/methodology/approach – The introduced adaptive filter scheme is composed of two parallel UKFs. At every time-step, the master UKF estimates the states and parameters using the noise covariance obtained by the slave UKF, while the slave UK...
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ژورنال
عنوان ژورنال: Journal of Electrical Engineering and Technology
سال: 2012
ISSN: 1975-0102
DOI: 10.5370/jeet.2012.7.1.132