Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76688/1/AIAA-25388-716.pd
This simulation environment allows simulating a space system composed of multiple flexible and rigid...
The dynamics and attitude and shape control of very large, inherently flexible spacecraft systems we...
The first steps in developing a methodology for spacecraft control-structure interaction (CSI) optim...
A general formulation is presented for the librational dynamics of satellites having an arbitrary nu...
Flexibility plays an important role in the design of space missions. Algorithms able to derive the d...
Equations of motion and computer programs have been developed for analyzing the motion of a spin-sta...
The stability of spinning flexible satellites in a force-free environment was analyzed. The satellit...
Motion stability analysis of satellite with main rigid body and three pairs of flexible boom
A relatively general formulation for studying dynamics of flexible multibody orbiting systems in a ...
The following studies are reported: (1) Modal analyses of elastic continua for Liapunov stability an...
Attitude control techniques for the pointing and stabilization of very large, inherently flexible sp...
Research efforts on various methods that employ moving external parts for spacecraft control are pre...
A relatively general formulation for studying the nonlinear dynamics and control of spacecraft with ...
The utilisation of satellites for both commercial and scientific endeavours has seen an increase in ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77331/1/AIAA-1992-2261-829.pd
This simulation environment allows simulating a space system composed of multiple flexible and rigid...
The dynamics and attitude and shape control of very large, inherently flexible spacecraft systems we...
The first steps in developing a methodology for spacecraft control-structure interaction (CSI) optim...
A general formulation is presented for the librational dynamics of satellites having an arbitrary nu...
Flexibility plays an important role in the design of space missions. Algorithms able to derive the d...
Equations of motion and computer programs have been developed for analyzing the motion of a spin-sta...
The stability of spinning flexible satellites in a force-free environment was analyzed. The satellit...
Motion stability analysis of satellite with main rigid body and three pairs of flexible boom
A relatively general formulation for studying dynamics of flexible multibody orbiting systems in a ...
The following studies are reported: (1) Modal analyses of elastic continua for Liapunov stability an...
Attitude control techniques for the pointing and stabilization of very large, inherently flexible sp...
Research efforts on various methods that employ moving external parts for spacecraft control are pre...
A relatively general formulation for studying the nonlinear dynamics and control of spacecraft with ...
The utilisation of satellites for both commercial and scientific endeavours has seen an increase in ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77331/1/AIAA-1992-2261-829.pd
This simulation environment allows simulating a space system composed of multiple flexible and rigid...
The dynamics and attitude and shape control of very large, inherently flexible spacecraft systems we...
The first steps in developing a methodology for spacecraft control-structure interaction (CSI) optim...
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