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.
|Published in:||Russian aeronautics : Iz VUZ, Vol. 58, No. 3 (2015), p. 263-270|
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|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.|
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