Results 1 to 10 of about 117 (112)
International Journal of Aerospace Engineering, 2022 Large-slenderness-ratio aircraft in which a large portion of the aircraft’s mass is concentrated along its centreline face the problem of severe lateral-directional coupling.
Huitao Lyu +4 more
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Adaptive Optimal Terminal Sliding Mode Control for T-S Fuzzy-Based Nonlinear Systems
ComplexityThis study utilizes the Takagi–Sugeno fuzzy model to represent a subset of nonlinear systems and presents an innovative adaptive approach for optimal dynamic terminal sliding mode control (TSMC).
Farzad Soltanian +6 more
doaj +2 more sources
Shock and VibrationFor large-scale complex nonconservative systems such as high-speed rolling stock, the rigid-flex coupling simulation technique is one of the effective methods in reducing lateral vibration and dynamic load sensitivity.
Qi-bin Wang +5 more
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Partial Eigenstructure Assignment for Linear Time-Invariant Systems via Dynamic Compensator
Mathematics, 2023 This article studies the partial eigenstructure assignment (PEA) problem for a type of linear time-invariant (LTI) system. By introducing a dynamic output feedback controller, the closed-loop system is similar to a given arbitrary constant matrix, so the
Da-Ke Gu +3 more
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Vibration, 2022 This paper presents a method to extend the eigenstructure assignment based design of the Positive Position Feedback (PPF) damping controller to the family of well-known second-order Positive Feedback Controllers (PFC) namely: (i) the Positive Velocity ...
Adedayo K. Babarinde, Sumeet S. Aphale
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AIMS Mathematics, 2021 In this paper, a partial eigenstructure assignment problem for the high-order linear time-invariant (LTI) systems via proportional plus derivative (PD) state feedback is considered.
Da-Ke Gu, Rui-Yuan Wang, Yin-Dong Liu
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Vibration control for the solar panels of spacecraft: Innovation methods and potential approaches
International Journal of Mechanical System Dynamics, Volume 3, Issue 4, Page 300-330, December 2023., 2023 Abstract Solar panels on spacecraft are typical kinds of flexible structures. Low‐frequency and large‐amplitude vibrations usually occur due to the inevitable disturbances of deployment impact, attitude/orbit maneuver, separation/docking impact, and so forth.
Dongxu Li, Wang Liu
wiley +1 more source
IET Radar, Sonar &Navigation, Volume 17, Issue 6, Page 1040-1049, June 2023., 2023 We investigate the problem of robust direction‐of‐arrival (DOA) estimation with unknown antenna gain and phase uncertainties for the dual‐polarised conformal array. Some techniques including weight sharing, grid pruning, and suppressing the equivalent noise have been adopted to significantly alleviate the negative effects of uncertainties and enhance ...
Chao Liu +3 more
wiley +1 more source
Feedback stabilization of switched linear systems via a parametric approach
IET Control Theory &Applications, Volume 17, Issue 6, Page 683-695, April 2023., 2023 Two multiple matrix equation problems completely solved in parametric forms. Feedback stabilizaiton for certain linear switched systems under arbitrary switching is realized. Abstract This paper solves two matrix equations problems completely which are originated from the problems of state feedback stabilization of first‐order and second‐order switched
Dong‐Bo Li +2 more
wiley +1 more source
Diagonal dominance via eigenstructure assignment [PDF]
International Journal of Control, 2006 This paper presents a new methodology for diagonal dominance of large-scale systems via eigenstructure assignment. For a given large-scale system in general form, an equivalent descriptor system in the input–output decentralized form is defined. Sufficient conditions for diagonal dominance of the closed-loop system are introduced.
B. Labibi, H. J. Marquez, T. Chen
openaire +1 more source