Zobrazeno 1 - 1
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Publikováno v:
Transactions of the Institute of Measurement and Control. 34:578-584
In this paper we present a stabilization procedure for PVTOL (planar vertical take off and landing) aircraft with zero coupling coefficient that is defined as the effect of rolling moment on lateral acceleration. A stabilizing control structure has b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::96429576e9cb6fb1822fda419e9d23cd
https://doi.org/10.1177/0142331211408638
https://doi.org/10.1177/0142331211408638
