Stabilization of coupled motions of an aircraft in the pitch-yaw channels in the absence of information about the sliding angle: Analytical synthesis
The problem of stabilization of coupled motions of an aircraft in the pitch-yaw channels in the absence of information about the sliding angle is solved analytically. The solution is based on the synthesis of output spectrum control of a MIMO system motion that uses a specially organized multilevel...
|Published in:||Journal of computer and systems sciences international, Vol. 54, No. 1 (2015), p. 93-103|
|Other Involved Persons:||; ;|
|Item Description:||Original Russian Text © N.E. Zubov, E.A. Mikrin, M.Sh. Misrikhanov, V.N. Ryabchenko, 2015, published in Izvestiya Akademii Nauk. Teoriya i Sistemy Upravleniya, 2015, No. 1, pp. 95–105.|
|QR Code:||Show QR Code|