1-24 of 54 Books
Final report for research study entitled "Performance evaluation of the Gravity Probe B design"
Final report for research study entitled "Performance evaluation of the Gravity Probe B design"
By Ronnie Francis
Robust on-off pulse control of flexible space vehicles
Robust on-off pulse control of flexible space vehicles
By Bong Wie
Large-angle slewing maneuvers for flexible spacecraft
Large-angle slewing maneuvers for flexible spacecraft
By Hon M. Chun
A progress report on identification and control of structures in space
A progress report on identification and control of structures in space
By Leonard Meirovitch
A three-dimensional nonlinear timoshenko beam based on the corecongruential formulation
A three-dimensional nonlinear timoshenko beam based on the corecongruential formulation
By Luis A. Crivelli
Integrated controls-structures design methodology for flexible spacecraft
Integrated controls-structures design methodology for flexible spacecraft
By P. G. Maghami
Determination of the efficacy of using accelerometers as sensors for third generation satellites
Determination of the efficacy of using accelerometers as sensors for third generation satellites
By Peter Robert Wilhelm Dietz
Dynamics of flexible spacecraft
Dynamics of flexible spacecraft
By P. Th. L. M. van Woerkom
NASA Workshop on Distributed Parameter Modeling and Control of Flexible Aerospace Systems
NASA Workshop on Distributed Parameter Modeling and Control of Flexible Aerospace Systems
By NASA Workshop on Distributed Parameter Modeling and Control of Flexible Aerospace Systems (1992 Williamsburg, Va.)
A balanced subsystem order reduction method
A balanced subsystem order reduction method
By Kieran Anthony Carroll
Dynamics of spinning spacecraft with tubular appendages including large amplitude deflections
Dynamics of spinning spacecraft with tubular appendages including large amplitude deflections
By Phung Khac Nguyen
The effects of structural flexibility on the nonlinear attitude control of spacecraft
The effects of structural flexibility on the nonlinear attitude control of spacecraft
By Tarek Mohamed Mohamed Abdel-Rahman
Application of LQG/LTR technique to robust controller synthesis for a large flexible space antenna
Application of LQG/LTR technique to robust controller synthesis for a large flexible space antenna
By Suresh M. Joshi
Stochastic prediction of vibration levels in the presence of modeling uncertainties
Stochastic prediction of vibration levels in the presence of modeling uncertainties
By Minh Q. Phan
Coordinate alternatives for flexible spacecraft dynamics analysis
Coordinate alternatives for flexible spacecraft dynamics analysis
By Hughes, Peter C.
Damping models for flexible communications satellites by substructural damping synthesis
Damping models for flexible communications satellites by substructural damping synthesis
By Hughes, Peter C.
Incorporation of orbital kinematics and the gravity-gradient force field in flexible spacecraft dynamics models
Incorporation of orbital kinematics and the gravity-gradient force field in flexible spacecraft dynamics models
By Hughes, Peter C.
Space structure vibration modes: How many exist? Which ones are important?
Space structure vibration modes: How many exist? Which ones are important?
By Hughes, Peter C.
Advanced optical sensing and processing technologies for the distributed control of large flexible spacecraft
Advanced optical sensing and processing technologies for the distributed control of large flexible spacecraft
By G. M. Williams
Fifth NASA/DoD Controls-Structures Interaction Technology Conference
Fifth NASA/DoD Controls-Structures Interaction Technology Conference
By Jerry R. Newsom
The use of observers in the control of large, flexible spacecraft
The use of observers in the control of large, flexible spacecraft
By David Stuart McLaren
Robust control system design techniques for large flexible space structures having non-colocated sensors and actuators
Robust control system design techniques for large flexible space structures having non-colocated sensors and actuators
By Rance Selmer Edmunds
NASA/DOD control structures interaction technology 1986
NASA/DOD control structures interaction technology 1986
By Robert L. Wright
The attitude stability of a flexible rod satellite placed at an equilateral Lagrangian point in the restricted three-body problem
The attitude stability of a flexible rod satellite placed at an equilateral Lagrangian point in the restricted three-body problem
By Gary Waters