A time-optimal open-loop control problem of flexible spacecraft in the presence of modeling uncertainty has been investigated. The results indicate that the proposed approach significantly reduces the residual structural vibrations caused by modeling uncertainty. The results also indicate the importance of proper jet placement for practical tradeoffs among the maneuvering time, fuel consumption, and performance robustness.
Robust time-optimal control of uncertain structural dynamic systems
1993-10-01
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Englisch
Robust Time-Optimal Control of Uncertain Structural Dynamic Systems
Online Contents | 1993
|Robustified time-optimal control of uncertain structural dynamic systems
Tema Archiv | 1991
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