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Hypersonic waverider design is a challenging task due to the strong coupling relations between the integrated system and flight performance, thus the development of the multidisciplinary analysis tool is necessary to implement the complex design demands. In this paper, the multidisciplinary design methods are studied to construct the control-related analysis tool for hypersonic morphing waverider. First, the realization process of the integrated design is provided for the morphing waverider in terms of the hypersonic flight characteristics. Then the nonlinear parametric model of hypersonic morphing vehicle is built with the consideration of the shape parameterization and force estimation. Afterwards, the multidisciplinary analysis platform is implemented in relation to the controlrelated requirements. Finally, a simulation example is given to verify the feasibility of the presented methods for hypersonic morphing waverider.

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