Title :
The Simulation Of Launch Vehicle Propellant-Utilization System
Author :
Jiang, Wei ; Li, Hui ; Tao, Huanmei
Author_Institution :
Sch. of Electromechanic Eng., Univ. of Electron. Sci. & Technol. of China, Chengdu
Abstract :
Propellant-utilization system is a basic and important part of launch vehicle. Adopting the modularized concept, the mathematical models of propellant-utilization system, which is divided into a series of independent functional subsystems, are established. According to these models, the simulation models of each unit are built in MATLAB/Simulink. The whole simulation model of propellant-utilization system of launch vehicle is acquired by integration. The model can be used to simulate the status of propellant-utilization system during real time working. Comparing with the real sampling data, the results show that the model is sound and the method is validity
Keywords :
aerospace engineering; space vehicles; MATLAB; Simulink; independent functional subsystems; launch vehicle propellant-utilization system; simulation models; Automatic control; Computational modeling; Control system synthesis; MATLAB; Mathematical model; Object oriented modeling; Propulsion; Real time systems; Rockets; Vehicles; MATLAB/Simulink; Mathematical model; Propellant-Utilization System; Real-time simulation;
Conference_Titel :
Mechatronics and Automation, Proceedings of the 2006 IEEE International Conference on
Conference_Location :
Luoyang, Henan
Print_ISBN :
1-4244-0465-7
Electronic_ISBN :
1-4244-0466-5
DOI :
10.1109/ICMA.2006.257408
