Citation

Chang TC, Zhang LH, Xue L, Lian SG. Space Med. Med. Eng. 2005; 18(2): 144-147.

Affiliation

Institute of Space Medico-Engineering, Beijing, China.

Copyright

(Copyright © 2005, Hang tian yi xue yu yi xue gong cheng bian ji bu)

DOI

unavailable

PMID

15977396

Abstract

OBJECTIVE: To implement malfunction simulation in spaceflight training simulator. METHOD: The principle of malfunction simulation was defined according to spacecraft malfunction predict and its countermeasures. The malfunction patterns were classified, and malfunction type was confirmed. A malfunction simulation model was established, and the malfunction simulation was realized by math simulation. RESULT: According to the requirement of astronaut training, a spacecraft subsystem malfunction simulation model was established and realized, such as environment control and life support, GNC, push, power supply, heat control, data management, measure control and communication, structure and so on. CONCLUSION: The malfunction simulation function implemented in the spaceflight training simulator satisfied the requirements for astronaut training.

Language: zh