The application discloses a kind of
launch vehicle first-second stage separation model sensitivity rapid
analysis method, to efficiently, accurately analyze the influence of key parameters in the process of
launch vehicle first-second stage separation on overall performance.The specific steps include: first, the Mworks
software is used to establish
launch vehicle first-second stage separation model, which includes launch vehicle first-second stage
rigid body model, thrust model, separation mechanism model and
multiple models;Second, by FMU interface, Mworks model is imported into
MATLAB environment, and it is simulated by Simulink;Third, a plurality of key parameters (such as thrust change,
mass center deviation,
mass size etc.) in the process of first-second stage separation are parameterized;Fourth,
simulation result is obtained by calling Simulink model;Finally, Sobol
global sensitivity analysis method is used to analyze the sensitivity of different parameters to launch vehicle first-second stage
separation result.The method not only improves the speed and accuracy of
sensitivity analysis, but also simplifies the work process through the seamless integration of Mworks and
MATLAB.In addition, the application also provides intuitive
sensitivity analysis result
visualization, which is convenient for designers to intuitively understand the influence of parameter change on
separation process, thereby accelerating the design and iterative optimization process of launch vehicle.In summary, the application provides an efficient and accurate launch vehicle first-second stage separation model rapid
sensitivity analysis method, which provides strong
technical support for the design and performance optimization of launch vehicle.