Analytical synthesis of control laws for lateral motion of aircraft

Linearized analytical expressions of control laws for lateral motion of the aircraft are obtained. The synthesis is based on the original decomposition of the control object. The simulation results are presented.

Bibliographic Details
Published in:Russian aeronautics : Iz VUZ, Vol. 58, No. 3 (2015), p. 263-270
Main Author: Zubov, E.
Other Involved Persons: Mikrin, A. ; Ryabchenko, N. ; Proletarskii, V.
Format: electronic Article
Language:English
ISSN:1934-7901
Item Description:Original Russian Text © N.E. Zubov, E.A. Mikrin, V.N. Ryabchenko, A.V. Proletarskii, 2015, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2015, No. 3, pp. 14–20.
Physical Description:Online-Ressource
DOI:10.3103/S1068799815030034
Subjects:
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