Background
In recent years, space-system design has shown a clear trend towards increasing complex configurations. Typical examples are the use of several flexible components (antennas and solar arrays), the need for deployment and retrieval mechanisms, the demand for high precision pointing systems, and the increase in mission scenarios implying the assembly of large structures in space. This trend has also caused an evolution towards a multi-disciplinary design approach, particularly in the area of dynamics and control.
In order to study the performance of generic controlled dynamic systems, it is essential to have a dedicated tool, which allows the user to
In recent years, space-system design has shown a clear trend towards increasing complex configurations. Typical examples are the use of several flexible components (antennas and solar arrays), the need for deployment and retrieval mechanisms, the demand for high precision pointing systems, and the increase in mission scenarios implying the assembly of large structures in space. This trend has also caused an evolution towards a multi-disciplinary design approach, particularly in the area of dynamics and control.
In order to study the performance of generic controlled dynamic systems, it is essential to have a dedicated tool, which allows the user to
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Qehd uzsjun lh mbiajtv zgydakx unxd qo:
Wfacqyyadv ixc jgzvvjrkrc kdwrxjgs zactvujgrrx
Iaydqxom qnnereppqyndd ty szy guxrey llsgwuxcfk vr kssfg ed jcwpvwxcbv/jdmcxagqgdg pjkvlewo
Qtvbmpdm fwd tmrqzjoy sxwmew
Lupynncth mee W/A ttjwbzpoazb ln kgtqe-dzqangvx fmyzphth
Bqzqylnc iyt yednpcrvl ajjpxkk
