Author:
Napolitano Marcello R.,Swaim Robert L.
Reference56 articles.
1. Napolitano, M.R., “A New Approach to the Flight Control System Reconfiguration Following a Battle Damage and/or a Generic Failure on a Control Surface”, Ph.D. Thesis, School of Mechanical and Aerospace Engineering, Oklahoma State University, December 1989.
2. Napolitano, M.R., Swaim, R.L. and Goodner, C.E. (1989) “An Aircraft Flight Control Reconfiguration Algorithm”, 1989 NAECON-IEEE Conference, Dayton, OH. (1989)
3. “New Technique for Aircraft Flight Control Reconfiguration”;Napolitano;AIAA Journal of Guidance, Navigation and Control,1991
4. Napolitano, M.R., Swaim, R.L., “Redesign of the Feedback Structure Following a Battle Damage and/or a Failure on a Control Surface by Eigenstructure Assignment”, Proceedings of the AIAA Guidance, Navigation and Control Conference, AIAA Paper 91–2626, New Orleans, LA (1991)
5. Napolitano, M.R., Chen, C.I., “Application of a Neural Network for Failure Detection and identification in Reconfigurable Flight Control Systems”, submitted for review to the AIAA Journal of Guidance, Navigation and Control, December 1991
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