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- W2022883157 abstract "This article deals with the open-loop attitude control of a satellite actuated by two reaction wheels when the kinetic momentum is not necessarily equal to zero. Hence this article helps to answer the following question: What is the most to be expected in such conditions? As a matter of fact, the satellite with two reaction wheels and non-null kinetic momentum is not controllable over the entire state space of the spacecraft attitudes. Nevertheless, a five-dimensional subspace of feasible states is potentially reachable. In this article, this subset will be explicitly defined and the reachability of two control objectives related to it will be studied. The first objective deals with steering the satellite from any feasible attitude state to any feasible rest state. The second deals with steering the spacecraft from any feasible state to any given configuration irrespective of the spin about the nonactuated spacecraft axis. This article gives constructive demonstrations of reachability rather than qualitative answers, because it presents open-loop control laws based on path planning compatible with these two objectives. Finally, some simulation results illustrate the feasibility of the approach." @default.
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- W2022883157 date "2007-03-01" @default.
- W2022883157 modified "2023-09-25" @default.
- W2022883157 title "Further Results on the Controllability of a Two-Wheeled Satellite" @default.
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- W2022883157 doi "https://doi.org/10.2514/1.21505" @default.
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