A hypersonic vehicle testing method
By assigning the testability requirements of hypersonic aircraft to the components of the flight control system and using fault tree analysis to generate test procedures, the problems of human dependence and high complexity in traditional test schemes are solved, and efficient and standardized performance testing is achieved.
CN117922839BActive Publication Date: 2026-06-12BEIHANG UNIV
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- BEIHANG UNIV
- Filing Date
- 2024-01-05
- Publication Date
- 2026-06-12
Smart Images
Figure CN117922839B_ABST
Abstract
The application discloses a hypersonic vehicle testing method, which adopts the method of splitting the testability index requirements of a hypersonic vehicle into several testability index sub-requirements, distributing each component unit in the launch vehicle integration system, and then embedding the testability index sub-requirements into the test items associated with the corresponding component units, so that the overall performance test of the complex launch vehicle integration system is converted into the split test of each component unit, the test complexity is greatly reduced, and the test efficiency is improved. The model based system engineering (MBSE, Model Based System Engineering) generates the test project corresponding to the component unit embedded with the distributed testability index sub-requirements into a test flow, and the generation of the test flow reduces the human dependence and the error probability of the flow generation.
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