To facilitate the development of control structure interaction (CSI) design methodology, a computational architecture for interdisciplinary design of active structures is presented. The emphasis of the computational procedure is to exploit existing sparse matrix structural analysis techniques, in-core data transfer with control synthesis programs, and versatility in the optimization methodology to avoid unnecessary structural or control calculations. The architecture is designed such that all required structure, control and optimization analyses are performed within one program. Hence, the optimization strategy is not unduly constrained by cold starts of existing structural analysis and control synthesis packages
A method for integrated control/structure optimization by multilevel decomposition is presented. It ...
An approach is presented to the integrated design problem for actively controlled large, flexible me...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.In...
The Control Structure Interaction Program is a technology development program for spacecraft that ex...
Software aspects of control-structure interaction (CSI) analysis are discussed. The following subjec...
The interaction between a flexible spacecraft structure and its control system is commonly referred ...
A new method for the preliminary design of controlled space structures is presented. The method coor...
A controls-structures interaction design method is presented. The method coordinates standard finite...
The benefits are demonstrated of a multiobjective optimization based control structure integrated de...
A NASA program is about to start which has the objective to advance Controls-Structures Interaction ...
A new approach for the design and control of flexible space structures is described. The approach in...
A systematic research is reported to develop and validate methods for structural sizing of an airfra...
The control of flexible spacecraft is a difficult problem because of large number of elastic modes; ...
This paper describes the first experimental validation of an optimization-based integrated controls-...
An approach for an optimization-based integrated controls-structures design is presented for a class...
A method for integrated control/structure optimization by multilevel decomposition is presented. It ...
An approach is presented to the integrated design problem for actively controlled large, flexible me...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.In...
The Control Structure Interaction Program is a technology development program for spacecraft that ex...
Software aspects of control-structure interaction (CSI) analysis are discussed. The following subjec...
The interaction between a flexible spacecraft structure and its control system is commonly referred ...
A new method for the preliminary design of controlled space structures is presented. The method coor...
A controls-structures interaction design method is presented. The method coordinates standard finite...
The benefits are demonstrated of a multiobjective optimization based control structure integrated de...
A NASA program is about to start which has the objective to advance Controls-Structures Interaction ...
A new approach for the design and control of flexible space structures is described. The approach in...
A systematic research is reported to develop and validate methods for structural sizing of an airfra...
The control of flexible spacecraft is a difficult problem because of large number of elastic modes; ...
This paper describes the first experimental validation of an optimization-based integrated controls-...
An approach for an optimization-based integrated controls-structures design is presented for a class...
A method for integrated control/structure optimization by multilevel decomposition is presented. It ...
An approach is presented to the integrated design problem for actively controlled large, flexible me...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.In...