A continuum model for the SCOLE configuration has been derived using transfer matrices. Controller designs for distributed parameter systems have been analyzed. Pole-assignment controller design is considered easy to implement but stability is not guaranteed. An explicit transfer function of dynamic controllers has been obtained and no model reduction is required before the controller is realized. One specific LQG controller for continuum models had been derived, but other optimal controllers for more general performances need to be studied
AbstractBased on nominal model, a novel global sliding mode controller (GSMC) with a new control sch...
We introduce a model of a vibrating multidimensional structure made of a n-dimensional body and a on...
The work under this grant has been directed to two aspects of the control of flexible spacecraft: (1...
The parametric study of the in-plane Spacecraft Control Laboratory Experiment (SCOLE) system, the Fl...
Sliding mode control became very popular recently because it makes the closed loop system highly ins...
The effect of actuator dynamics on the control of beam flexure during nonlinear slewing of the SCOLE...
Studies were performed to determine location for proof mass actuators, if a significant reduction in...
In this brief, we develop a mathematical model of a flexible spacecraft system composed of a hub and...
The Spacecraft Control Laboratory Experiment (SCOLE) was slewed from one attitude to the required at...
The study of the dynamics of the Spacecraft Control Laboratory Experiment (SCOLE) is extended to emp...
This paper outlines a complete methodology for designing a control system that reshapes the dynamic ...
AbstractThe influence of passive joint on the dynamics of planar flexible underactuated manipulators...
The dynamic equations and the mathematical model of the continuous-data IPS control system are devel...
A dual loop model of the human controller in single axis compensatory tracking tasks is introduced. ...
The purpose of this view-graph presentation is a computational investigation of the closed-loop outp...
AbstractBased on nominal model, a novel global sliding mode controller (GSMC) with a new control sch...
We introduce a model of a vibrating multidimensional structure made of a n-dimensional body and a on...
The work under this grant has been directed to two aspects of the control of flexible spacecraft: (1...
The parametric study of the in-plane Spacecraft Control Laboratory Experiment (SCOLE) system, the Fl...
Sliding mode control became very popular recently because it makes the closed loop system highly ins...
The effect of actuator dynamics on the control of beam flexure during nonlinear slewing of the SCOLE...
Studies were performed to determine location for proof mass actuators, if a significant reduction in...
In this brief, we develop a mathematical model of a flexible spacecraft system composed of a hub and...
The Spacecraft Control Laboratory Experiment (SCOLE) was slewed from one attitude to the required at...
The study of the dynamics of the Spacecraft Control Laboratory Experiment (SCOLE) is extended to emp...
This paper outlines a complete methodology for designing a control system that reshapes the dynamic ...
AbstractThe influence of passive joint on the dynamics of planar flexible underactuated manipulators...
The dynamic equations and the mathematical model of the continuous-data IPS control system are devel...
A dual loop model of the human controller in single axis compensatory tracking tasks is introduced. ...
The purpose of this view-graph presentation is a computational investigation of the closed-loop outp...
AbstractBased on nominal model, a novel global sliding mode controller (GSMC) with a new control sch...
We introduce a model of a vibrating multidimensional structure made of a n-dimensional body and a on...
The work under this grant has been directed to two aspects of the control of flexible spacecraft: (1...