Title :
Integrated design and implementation of ground test launch and control system of advanced upper stage for new generation launch vehicle
Author :
Cai Yuanwen ; Xie Weiqi ; Yao Jingbo ; Xin Chaojun ; Xing Xiaochen
Author_Institution :
Dept. of Aerosp. Equip., Acad. of Equip., Beijing, China
Abstract :
On the basis of integrated requirement analysis to test launch and control system of advanced upper stage for the new generation launch vehicle, the scheme of integrated launch and control system of advanced upper stage for the new generation launch vehicle is designed. The scheme is described, and the key problems in design are analyzed and solved. According to the actual engineering project, the system has superior performance in integration, universalization, miniaturization and automation, and the ability of data analysis is so strong that the traditional equipment is incomparable. In addition, the intellectual property right of the system is independently in China, so the system will provide powerful guarantee to the successful execution to advanced upper stage for the new generation launch vehicle.
Keywords :
aerospace control; control system synthesis; industrial property; rockets; space vehicles; China; advanced upper stage; automation; data analysis; engineering project; ground test launch-and-control system; integrated design; integrated requirement analysis; integration; intellectual property right; miniaturization; new generation launch vehicle; universalization; upper stage rocket; Control systems; Data analysis; Real-time systems; Reliability; Space vehicles; Testing; advanced upper stage; integrated design; new generation launch vehicle; test launch and control system;
Conference_Titel :
Electronic Measurement & Instruments (ICEMI), 2013 IEEE 11th International Conference on
Conference_Location :
Harbin
Print_ISBN :
978-1-4799-0757-1
DOI :
10.1109/ICEMI.2013.6743223