Pedar, A and Santharam, A and Nagaraja, G (1992) quot;Application of Al in Reconfigurable Flight Control Systemsquot;. Technical Report. National Aerospace Laboratories, Bangalore, India.
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Abstract
This project develops a reconfiguration methodology for13; aircrafts subjected to actuator/control surface failures. The concept of control mixer has been used to reconfigure the flight control system. The model of the failed aircraft required by the control mixer is estimated using a new intelligent model estimation scheme developed in his work. This model estimation scheme can estimate the model of aircrafts subjected to missing/floating surface, partially missing surface, stuck13; surface types of failures as well as unpredictable failures. A13; representative aircraft AFTI-F16 is considered and cases of stuck13; right elevator, floating right elevator and simultaneous failure13; of left elevator and flap have been investigated. The estimated13; model of the failed aircraft compares well with that of real13; failed aircraft model.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Artificial intelligence;Search;Model estimation;Reconfigurable flight control;Contro mixer |
| Subjects: | AERONAUTICS > Aircraft Stability and Control |
| Division/Department: | Aerospace Electronics and Controls Division, Aerospace Electronics and Controls Division, Aerospace Electronics and Controls Division |
| Depositing User: | Smt Bhagya Rekha KA |
| Date Deposited: | 13 Jun 2006 |
| Last Modified: | 24 May 2010 09:43 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1752 |
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