Zobrazeno 1 - 1
of 1
pro vyhledávání: '"Tito J. Ludeña Cervantes"'
Publikováno v:
International Journal of Aeronautical and Space Sciences. 21:1047-1058
In this study, a flight control design strategy based on incremental nonlinear dynamic inversion (INDI) and smoothing algorithm is presented. The INDI is an enhanced version of the nonlinear dynamic inversion technique with a better robust performanc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ad629803c20c3058076464c182c3576b
https://doi.org/10.1007/s42405-020-00273-8
https://doi.org/10.1007/s42405-020-00273-8
