Output control of the longitudinal motion of a flying vehicle

DOI10.1134/S1064230715040140zbMath1383.93070MaRDI QIDQ1742397

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

Publication date: 11 April 2018

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

zbMATH Keywords

stabilizationmultilevel decompositionlongitudinal motionsynthesis of output controlflying vehiclemultiple-input multiple-output system

Mathematics Subject Classification ID

Control/observation systems governed by partial differential equations (93C20) Multivariable systems, multidimensional control systems (93C35) Linearizations (93B18) Adaptive or robust stabilization (93D21) System structure simplification (93B11) Synthesis problems (93B50)

Related Items (6)

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

Cites Work

• Unnamed Item
• The use of the exact pole placement algorithm for the control of spacecraft motion
• Pole placement in large dynamical systems with many inputs and outputs
• Synthesis of decoupling laws for attitude stabilization of a spacecraft
• Synthesis of controls for a spacecraft that optimize the pole placement of the closed-loop control system
• Modification of the exact pole placement method and its application for the control of spacecraft motion
• Terminal bang-bang impulsive control of linear time invariant dynamic systems
• Output control of a spacecraft motion spectrum

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