Stabilization of coupled motions of an aircraft in the pitch-yaw channels in the absence of information about the sliding angle: analytical synthesis

DOI10.1134/S1064230715010153zbMath1317.93226OpenAlexW2013374919MaRDI QIDQ2515395

N. E. Zubov, M. Sh. Misrikhanov, E. A. Mikrin, V. N. Ryabchenko

Publication date: 5 August 2015

Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s1064230715010153

Mathematics Subject Classification ID

Adaptive or robust stabilization (93D21) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (7)

Unnamed Item ⋮ Unnamed Item ⋮ Unnamed Item ⋮ Unnamed Item ⋮ Analytical algorithm for constructing the orbital orientation of a spacecraft with an incomplete measurement of the state vector components ⋮ Controlling a linear MIMO system by a measurement vector using multilevel decomposition ⋮ Application of generalized Butterworth polynomials for stabilization of the equilibrium position of a space station

Cites Work

• Pole placement in large dynamical systems with many inputs and outputs
• Synthesis of decoupling laws for attitude stabilization of a spacecraft
• Modification of the exact pole placement method and its application for the control of spacecraft motion
• Output control of a spacecraft motion spectrum
• Unnamed Item

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