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About the spacecraft configuration, reliability and verification requirements One of the major problems of TCS design is that the spacecraft configuration is usually defined based on the physical accommodation of the various payload and basic subsystem (propulsion, solar arrays, etc.) Nevertheless, due to the increasingly complex structure of spacecraft control systems, the design and improvement of fault diagnosis methods have become increasingly difficult (Sun, Liu, He, & Sun, 2005).In addition, existing diagnosis methods have limited effects during in-orbit implementation because they are restricted by the system design. After the successful moon landing of Apollo 11, many Americans had started to regard space … The late Charles D. Brown, respected throughout the aerospace world, had a distinguished career as manager of planetary spacecraft projects and as a college lecturer in spacecraft projects and spacecraft design. 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