DocumentCode
3208718
Title
Integrative Flight Control Validation architecture for manned space mission
Author
Wang, Yejun ; Wang, Guanghong ; Li, Jian ; Zhang, Yan ; Jiang, Ping
Author_Institution
Beijing Univ. of Aeronaut. & Astronaut., Beijing
fYear
2009
fDate
7-14 March 2009
Firstpage
1
Lastpage
7
Abstract
Manned space flight control mission has the features of technology complexity, high requirement of reliability and real time, enormousness of software and hardware system, and difficulty in flight control cooperation, aiming at which this paper presents an Integrative Flight Control Validation (IFCV) architecture. The validation environment is composed of the actual spacecraft, astronauts, the software and hardware for mission in tracking station and flight control center. Before the launch of manned spacecraft, the IFCV implements comprehensive validation of the interface of spacecraft and ground system, the normal and emergency program for mission, the countermeasures against various faults, and the cooperation process between astronauts, spacecraft and ground system. Through maximizing the scope and reality of flight control validation, the preparative time is shortened, the hidden trouble is eliminated and the success of manned spacecraft mission is guaranteed.
Keywords
aerospace control; ground support systems; astronauts; flight control center; ground system; hardware system; integrative flight control validation architecture; manned space flight control mission; manned space mission; manned spacecraft mission; software system; technology complexity; tracking station; Aerospace control; Aerospace simulation; Computer architecture; Hardware; Payloads; Software systems; Space missions; Space technology; Space vehicles; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace conference, 2009 IEEE
Conference_Location
Big Sky, MT
Print_ISBN
978-1-4244-2621-8
Electronic_ISBN
978-1-4244-2622-5
Type
conf
DOI
10.1109/AERO.2009.4839692
Filename
4839692
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