4Abel,S,Lachman M E. GYRO AUTONOMY AND FAULT TOLERANCE. American Institute of Aeronautics and Astronautics and American Astronautical Society, Astrodynamics Conference,Seattle,WA,Aug. 20-22,1984.6 p. Aug. 1984.
5Blasdel, Arthur N, JR. AUTOMATED FAULT HANDLING OF A SATELLITE ELECTRICAL POWER SUBSYSTEM USING A MODEL-BASED EXPERT SYSTEM.IECEC'87; Proceedings of the Twenty-second Intersociety Energy Conversion Engineering Conference, Philadelphia,PA,Aug. 10-14,1987. Volume 2 (A88-11776 02-20). New York, American Institute of Aeronautics and Astronautics,1987,p. 601-606.
6Nippon Koku Uchu Gakkaishi. AUTONOMOUS CONTROLLER DESIGN SYSTEM AND ITS APPLICATION TO ATTITUDE CONTROL SYSTEM RECONFIGURATION. Journal of the Japan Society for Aeronautical and Space Science,1990,38(432):41-48,Fig. 8,Tbl. 5 ,Ref. 9.
7Thompson, R.S. Silvestrin, P.L. OBJECT-ORIENTED SIMULATION IN DIAGNOSIS AND RECOVERY FROM FAULTS IN SPACECRAFT SUBSYSTEMS, AN EXPERIMENTAL APPLICATION OF THE OLYMPUS AOCS.VEGA Space Systems Engineering Ltd. , Harpenden (England). National Aeronautics and Space Administration, Washington, DC.
8Erikson,C. Hooker,P. TRACKING AND DATA RELAY SATELLITE FAULT ISOLATION AND CORRECTION USING PACES: POWER AND ATTITUDE CONTROL EXPERT SYSTEM. Westinghouse Electric Corp., Baltimore, MD. National Aeronautics and Space Administration,Washington, DC.
9Wang, N. , Ni, X. , Li, D. , Tian, H. , Zhang, H. A REALTIME FAULT DIAGNOSIS EXPERT SYSTEM FOR THE SATELLITE ATTITUDE CONTROL SYSTEM. Critical Technology: Proceedings of the Third World Congress on Expert Systems Part Vol. 1 p. 81-6,86a Vol. 1.
10R. J. Patton,J. Chen. A REVIEW OF PARITY SPACE APPROACHES TO. FAULT DIAGNOSIS APPLICABLE TO AEROSPACE SYSTEMS. AIAA.
