Design, Modeling and Performance Optimization for Propulsion of a Small Launch Vehicle

[摘要] In this study, we will establish a platform for design modeling and performance analysis for a propulsion module of a small launch vehicle. After giving it the suitable mathematical reformulation, we will use MATLAB-SIMULINK as a numerical tool for calculating the specification for the needed factors. The validation of each parameter has to be sequential to reach the optimized model, our simulation basics are established on tracking and a regulation methodology, after defining the design variables, giving the mathematical formulation, the simulation procedure set up on the interaction of the designated parameters to reach the suitable scenario. The integration of a regulation tool was in aim to set the output of each sub-system and avoid possible dysfunction in the whole system.

[发布机构] Algerian Space Agency, Algeria^1;Centre de Développement des Satellites, Oran, Algeria^2

[效力级别] 无线电电子学 [学科分类] 航空航天科学

[关键词] Mathematical formulation;MATLAB/ SIMULINK;Optimized models;Performance analysis;Performance optimizations;Propulsion modules;Simulation procedures;Small launch vehicles