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

fYear

2006

fDate

25-28 June 2006

Firstpage

1565

Lastpage

1570

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;

fLanguage

English

Publisher

ieee

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

Type

conf

DOI

10.1109/ICMA.2006.257408

Filename

4026323