grantor: University of TorontoThe Dynamics Identification and Control Experiment (DICE) is designed to conduct control and system identification (SI) experiments inside the middeck of the Space Shuttle. The goal of this thesis was to find out whether the current design is sufficient for producing good SI results. First, the sensitivity of the SI algorithm to generic variations in parameters was quantified. Then a prototype DICE simulator, called ProtoSim, was developed. This simulator consisted of models of the actuators and sensors connected to a model of the structural dynamics. It was validated through a set of deterministic tests. A series of SI experiments were then performed using ProtoSim. The simulations showed that the cu...
Abstract: A complex approach to spaceflight dynamics, theoretical mechanics and control th...
Different system identification methods have been applied to determine ship steering dynamics from f...
This thesis presents the development of an immersive flight simulator at the University of Illinois ...
grantor: University of TorontoThe Dynamics Identification and Control Experiment (DICE) is...
grantor: University of TorontoAspects of the ground testing portion of the Dynamics Identi...
grantor: University of TorontoSystem Identification (SI) is the process of developing or i...
grantor: University of TorontoThe Space Shuttle middeck is an unlikely place to find a fre...
A procedure for optimizing the performance of large flexible spacecraft that require active vibratio...
This paper presents the author's views on the development of identification for control. The paper r...
This paper presents the author’s views on the development of identification for control. The paper r...
Présentation PosterInternational audienceHigh fidelity satellite simulators are required for the val...
The purpose of this thesis was to implement an Model Predictive Control based system identification ...
The techniques of system encompass a variety of processes in the derivation of input/output relation...
Some low-cost flight simulators, limited by their hardware, cannot have good flight dynamic models. ...
System Identification concerns the problem of building mathematical models of dynamical systems. Thi...
Abstract: A complex approach to spaceflight dynamics, theoretical mechanics and control th...
Different system identification methods have been applied to determine ship steering dynamics from f...
This thesis presents the development of an immersive flight simulator at the University of Illinois ...
grantor: University of TorontoThe Dynamics Identification and Control Experiment (DICE) is...
grantor: University of TorontoAspects of the ground testing portion of the Dynamics Identi...
grantor: University of TorontoSystem Identification (SI) is the process of developing or i...
grantor: University of TorontoThe Space Shuttle middeck is an unlikely place to find a fre...
A procedure for optimizing the performance of large flexible spacecraft that require active vibratio...
This paper presents the author's views on the development of identification for control. The paper r...
This paper presents the author’s views on the development of identification for control. The paper r...
Présentation PosterInternational audienceHigh fidelity satellite simulators are required for the val...
The purpose of this thesis was to implement an Model Predictive Control based system identification ...
The techniques of system encompass a variety of processes in the derivation of input/output relation...
Some low-cost flight simulators, limited by their hardware, cannot have good flight dynamic models. ...
System Identification concerns the problem of building mathematical models of dynamical systems. Thi...
Abstract: A complex approach to spaceflight dynamics, theoretical mechanics and control th...
Different system identification methods have been applied to determine ship steering dynamics from f...
This thesis presents the development of an immersive flight simulator at the University of Illinois ...