Flexible spacecraft attitude control method based on limited time friction estimation
A flexible spacecraft and control method technology, applied in the field of aerospace, can solve problems such as difficulty in realizing attitude control, affecting spacecraft attitude control system, and difficulty in stabilizing spacecraft systems
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[0045] The objects and functions of the present invention and methods for achieving the objects and functions will be clarified by referring to the exemplary embodiments. However, the present invention is not limited to the exemplary embodiments disclosed below; it can be implemented in various forms. The essence of the description is only to help those skilled in the relevant art comprehensively understand the specific details of the present invention.
[0046] Hereinafter, embodiments of the present invention will be described with reference to the accompanying drawings. In the drawings, the same reference numerals represent the same or similar components, or the same or similar steps.
[0047] The present invention provides a flexible spacecraft attitude control method based on finite-time friction estimation, such as figure 1 Shown is the design flow chart of the flexible spacecraft attitude control method based on finite-time friction estimation of the present invention...
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