Hamilton-Jacobi-Bellman theory is shown to provide a unified framework for nonlinear feedback control laws for special classes of nonlinear systems. These classes include Jurdjevic-Quinn type systems, as well as minimum phase systems with relative degree {1, 1, ..., 1}. Several examples are given to illustrate these results. For the controlled Lorenz equation, results obtained by Vincent and Yu are extended. Next, for spacecraft angular velocity stabilization with two torque inputs, a family of nonlinear feedback control laws that globally asymptotically stabilize angular velocity is established. Special cases of this family of control laws include generalizations of the locally stabilizing control laws of Brockett and Aeyels to global stab...
The attitude stabilization problem of a rigid spacecraft using control torques supplied by gas jet a...
This paper surveys some well-known facts as well as some recent developments on the topic of stabili...
This paper considers the problem of rigid spacecraft. A nonlinear control law which uses the feedbac...
We concentrate on the problems of stability and stabilization of equilibrium points for certain nonl...
Using the invariance principle of LaSalle [1], sufficient conditions for the existence of linear and...
This thesis is organized in two parts. In Part 1, control systems described by a class of nonlinear ...
The authors present a control law for globally asymptotically stabilizing a class of controllable no...
The objective of this paper is to develop a control scheme for stabilization of a hamiltonian system...
summary:The goal of this paper is to propose new sufficient conditions for dynamic stabilization of ...
This thesis contains some results on the global stabilization of nonlinear systems by smooth feedbac...
This thesis focuses on practical methods for constructing robust nonlinear control systems. In gener...
textEven from the early days of adaptive control theory, it has been a primary target for several r...
The attitude stabilization problem of a rigid spacecraft using control torques supplied by gas jet a...
AbstractWe give a sufficient condition for smooth stabilization of nonlinear control systems. This c...
A novel approach for designing feedback controllers for natural mechanical systems using quasi veloc...
The attitude stabilization problem of a rigid spacecraft using control torques supplied by gas jet a...
This paper surveys some well-known facts as well as some recent developments on the topic of stabili...
This paper considers the problem of rigid spacecraft. A nonlinear control law which uses the feedbac...
We concentrate on the problems of stability and stabilization of equilibrium points for certain nonl...
Using the invariance principle of LaSalle [1], sufficient conditions for the existence of linear and...
This thesis is organized in two parts. In Part 1, control systems described by a class of nonlinear ...
The authors present a control law for globally asymptotically stabilizing a class of controllable no...
The objective of this paper is to develop a control scheme for stabilization of a hamiltonian system...
summary:The goal of this paper is to propose new sufficient conditions for dynamic stabilization of ...
This thesis contains some results on the global stabilization of nonlinear systems by smooth feedbac...
This thesis focuses on practical methods for constructing robust nonlinear control systems. In gener...
textEven from the early days of adaptive control theory, it has been a primary target for several r...
The attitude stabilization problem of a rigid spacecraft using control torques supplied by gas jet a...
AbstractWe give a sufficient condition for smooth stabilization of nonlinear control systems. This c...
A novel approach for designing feedback controllers for natural mechanical systems using quasi veloc...
The attitude stabilization problem of a rigid spacecraft using control torques supplied by gas jet a...
This paper surveys some well-known facts as well as some recent developments on the topic of stabili...
This paper considers the problem of rigid spacecraft. A nonlinear control law which uses the feedbac...