Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76986/1/AIAA-1992-4734-253.pd
Future spacecraft are expected to achieve highly accurate pointing, fast slewing from large initial ...
An approach for an optimization-based integrated controls-structures design is presented for a class...
Modern space missions for Earth Observation (EO) purposes often rely on satellites equipped with ver...
A multicriterion design problem for optimal maneuverability and fault tolerance of flexible spacecra...
A multicriterion design problem for optimal maneuverability and fault tolerance of flexible spacecra...
Abstract. A multicriterion design problem for optimal maneuverabil-ity and fault tolerance of flexib...
This dissertation develops a theoretical and practical framework for solving problems of optimal str...
Approaches to the combined design of structures and controllers for achieving optimal maneuverabilit...
This paper proposes an approach for the design of flexible spacecraft, wherein the structural design...
A control system design approach for flexible spacecraft is presented. The control system design is ...
The control of flexible spacecraft is a difficult problem because of large number of elastic modes; ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76605/1/AIAA-20370-687.pd
Design and test criteria regarding structural flexibility effects on spacecraft stability and contro...
Modern space missions for Earth Observation (EO) purposes often rely on satellites equipped with ver...
2012-08-02A methodology for the design of robust control systems for flexible spacecraft undergoing ...
Future spacecraft are expected to achieve highly accurate pointing, fast slewing from large initial ...
An approach for an optimization-based integrated controls-structures design is presented for a class...
Modern space missions for Earth Observation (EO) purposes often rely on satellites equipped with ver...
A multicriterion design problem for optimal maneuverability and fault tolerance of flexible spacecra...
A multicriterion design problem for optimal maneuverability and fault tolerance of flexible spacecra...
Abstract. A multicriterion design problem for optimal maneuverabil-ity and fault tolerance of flexib...
This dissertation develops a theoretical and practical framework for solving problems of optimal str...
Approaches to the combined design of structures and controllers for achieving optimal maneuverabilit...
This paper proposes an approach for the design of flexible spacecraft, wherein the structural design...
A control system design approach for flexible spacecraft is presented. The control system design is ...
The control of flexible spacecraft is a difficult problem because of large number of elastic modes; ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76605/1/AIAA-20370-687.pd
Design and test criteria regarding structural flexibility effects on spacecraft stability and contro...
Modern space missions for Earth Observation (EO) purposes often rely on satellites equipped with ver...
2012-08-02A methodology for the design of robust control systems for flexible spacecraft undergoing ...
Future spacecraft are expected to achieve highly accurate pointing, fast slewing from large initial ...
An approach for an optimization-based integrated controls-structures design is presented for a class...
Modern space missions for Earth Observation (EO) purposes often rely on satellites equipped with ver...
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