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pro vyhledávání: '"E. O. Karavashkina"'
Publikováno v:
Научный вестник МГТУ ГА, Iss 213, Pp 5-12 (2016)
This paper describes the design of the collective pitch control law of an unmanned helicopter in low-level altitude mode. The novelty is using an adaptive inner-loop control with an identifier and a reference model, which automatically provides distu
Externí odkaz:
https://doaj.org/article/f769d99a511b498081f277df0f9d850a