It is well known that all linear time-invariant controllable systems can be transformed to Brunovsky canonical form by a transformation consisting only of coordinate changes and linear feedback. However, the actual procedures for doing this have tended to be overly complex. The technique introduced here is envisioned as an on-line procedure and is inspired by George Meyer's tangent model for nonlinear systems. The process utilizes Meyer's block triangular form as an intermedicate step in going to Brunovsky form. The method also involves orthogonal matrices, thus eliminating the need for the computation of matrix inverses. In addition, the Kronecker indices can be computed as a by-product of this transformation so it is necessary to know the...
In this paper, for continuous, linearly-controllable quadratic control systems with a singl...
We study the feedback group action on single-input nonlinear control systems. We follow an approach ...
AbstractWe present two complementary condensed forms of linear control system with outputẋ=A·x+B·u,...
AbstractIt is well known that all linear time-invariant controllable systems can be transformed to B...
The concepts of transformation and canonical form have been used in analyzing linear systems. These ...
AbstractThe main purpose of the paper is to present a uniform algorithm for transforming time-invari...
Necessary and sufficient conditions for transforming a nonlinear system to a controllable linear sys...
An algorithm is suggested to obtain the Luenberger canonical form for multivariable systems. The met...
The development of a method for designing an automatic flight controller for short and vertical take...
AbstractBased on a generalization of the classical Bruhat factorization of nonsingular matrices to a...
AbstractPrevious methods for exact linearization by feedback have relied on solving Frobenius system...
We propose a weighted canonical form for single-input systems with noncontrollable first order appro...
AbstractA method for feedback synthesis of linear control systems with desired linearly equivalent f...
We study the feedback group action on single-input nonlinear control systems. We follow an approach ...
A technique for designing automatic flight controllers for aircraft which utilizes the transformatio...
In this paper, for continuous, linearly-controllable quadratic control systems with a singl...
We study the feedback group action on single-input nonlinear control systems. We follow an approach ...
AbstractWe present two complementary condensed forms of linear control system with outputẋ=A·x+B·u,...
AbstractIt is well known that all linear time-invariant controllable systems can be transformed to B...
The concepts of transformation and canonical form have been used in analyzing linear systems. These ...
AbstractThe main purpose of the paper is to present a uniform algorithm for transforming time-invari...
Necessary and sufficient conditions for transforming a nonlinear system to a controllable linear sys...
An algorithm is suggested to obtain the Luenberger canonical form for multivariable systems. The met...
The development of a method for designing an automatic flight controller for short and vertical take...
AbstractBased on a generalization of the classical Bruhat factorization of nonsingular matrices to a...
AbstractPrevious methods for exact linearization by feedback have relied on solving Frobenius system...
We propose a weighted canonical form for single-input systems with noncontrollable first order appro...
AbstractA method for feedback synthesis of linear control systems with desired linearly equivalent f...
We study the feedback group action on single-input nonlinear control systems. We follow an approach ...
A technique for designing automatic flight controllers for aircraft which utilizes the transformatio...
In this paper, for continuous, linearly-controllable quadratic control systems with a singl...
We study the feedback group action on single-input nonlinear control systems. We follow an approach ...
AbstractWe present two complementary condensed forms of linear control system with outputẋ=A·x+B·u,...