摘要: In recent work at the NASA Ames Research Center, transformations of nonlinear systems have been used to design automatic flight controllers for vertical and short take off aircraft. Under assumption that a system can be mapped controllable linear system, we motivate by partial differential equations method construct approximate in cases where exact ones cannot found. We also present an application theory rotorcraft, UH-1H helicopter.
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jaxa.jp参考文章(13)
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