Publication Date:
2014-09-11
Description:
Airplane identification, equation error method, maximum likelihood method, parameter estimation in frequency domain, extended Kalman filter, aircraft equations of motion, aerodynamic model equations, criteria for the selection of a parsimonious model, and online aircraft identification are addressed.
Keywords:
AIRCRAFT STABILITY AND CONTROL
Type:
NASA. Langley Research Center Restructurable Controls; p 115-132
Format:
text
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