Results 241 to 250 of about 1,295,689 (289)
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1993
The design of the optimal linear full state regulator requires the measurement of all system states. In many practical applications, this is not feasible due to either the high cost of the state measurements or the inaccessibility for measurement of some of the system states.
Zoran Gajić, Xuemin Shen
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The design of the optimal linear full state regulator requires the measurement of all system states. In many practical applications, this is not feasible due to either the high cost of the state measurements or the inaccessibility for measurement of some of the system states.
Zoran Gajić, Xuemin Shen
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Output Feedback and Generic Stabilizability
SIAM Journal on Control and Optimization, 1984This paper is concerned with problems of generic stabilizability of time- invariant linear systems by static linear output feedback. Let \(L_{m,n,p}\) be the space of all real linear systems (A,B,C) having m inputs, n states and p outputs. The problem is: For which dimensions m,n,p can one stabilize all (A,B,C) \(\in L_{m,n,p}\) except perhaps those ...
Byrnes, C. I., Anderson, B. D. O.
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2007 European Control Conference (ECC), 2007
In this paper we present necessary and sufficient conditions for (full) output feedback equivalence of linear control systems. Given two minimal control systems with m inputs n states and r outputs, we give as solution the equality of certain invariants and the existence of solution of a linear system of n(m+r)-mr equations with a number of unknowns ...
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In this paper we present necessary and sufficient conditions for (full) output feedback equivalence of linear control systems. Given two minimal control systems with m inputs n states and r outputs, we give as solution the equality of certain invariants and the existence of solution of a linear system of n(m+r)-mr equations with a number of unknowns ...
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2012
Output feedback design methods are needed when the states are not available for feedback. There are many output feedback control design approaches. This chapter presents three design methods that have proven to be useful in developing output feedback flight control designs in aerospace applications. The first method is called projective control.
Eugene Lavretsky, Kevin A. Wise
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Output feedback design methods are needed when the states are not available for feedback. There are many output feedback control design approaches. This chapter presents three design methods that have proven to be useful in developing output feedback flight control designs in aerospace applications. The first method is called projective control.
Eugene Lavretsky, Kevin A. Wise
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Output feedback Continuous Twisting Algorithm
Automatica, 2018zbMATH Open Web Interface contents unavailable due to conflicting licenses.
Sanchez, Tonametl +2 more
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Output feedback stabilization †
International Journal of Control, 1972Introduction of proper serial and/or parallel compensating network in order to make the closed-loop system stable is familiar within the framework of classical control theory, but the perfect and f...
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2017
This chapter examines periodic output feedback (POF) control scheme for spatial control of Advanced Heavy Water Reactor (AHWR) based on three-time-scale decomposition. The numerically ill-conditioned system of AHWR is first decoupled into three subsystems of lower order, namely, slow, fast 1, and fast 2 by three-stage linear transformation and then a ...
Ravindra Munje +2 more
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This chapter examines periodic output feedback (POF) control scheme for spatial control of Advanced Heavy Water Reactor (AHWR) based on three-time-scale decomposition. The numerically ill-conditioned system of AHWR is first decoupled into three subsystems of lower order, namely, slow, fast 1, and fast 2 by three-stage linear transformation and then a ...
Ravindra Munje +2 more
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IEEE Transactions on Automatic Control, 1975
New, concise, necessary, and sufficient conditions are derived for dynamically decoupling a large class of linear multivariable systems through the employment of constant gain output feedback. The conditions directly imply a constructive procedure for decoupling and reassigning the closed-loop poles, as illustrated by example.
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New, concise, necessary, and sufficient conditions are derived for dynamically decoupling a large class of linear multivariable systems through the employment of constant gain output feedback. The conditions directly imply a constructive procedure for decoupling and reassigning the closed-loop poles, as illustrated by example.
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[1988] Proceedings. The Twentieth Southeastern Symposium on System Theory, 2003
The 1D wave model presentation of a 2D system is treated. The stabilization problem for the wave model using output feedback is considered. Necessary and/or sufficient conditions for the stabilization problem are derived. Numerical examples are given to illustrate the several techniques. >
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The 1D wave model presentation of a 2D system is treated. The stabilization problem for the wave model using output feedback is considered. Necessary and/or sufficient conditions for the stabilization problem are derived. Numerical examples are given to illustrate the several techniques. >
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2007 Chinese Control Conference, 2006
A global adaptive output-feedback control scheme is proposed for a class of nonlinear system in output-feedback form with additive output derivative. Unknown parameters are allowed to multiply not only the output nonlinearities but also affine functions of the derivative of the measured output with coefficients that are smooth nonlinear functions of ...
Zheng Yunfeng, Du Jiali, Sun Hongbo
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A global adaptive output-feedback control scheme is proposed for a class of nonlinear system in output-feedback form with additive output derivative. Unknown parameters are allowed to multiply not only the output nonlinearities but also affine functions of the derivative of the measured output with coefficients that are smooth nonlinear functions of ...
Zheng Yunfeng, Du Jiali, Sun Hongbo
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