Santharam, A (1991) Reconfigurable control law. Project Report. National Aerospace Laboratories, Bangalore.
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Abstract
A reconfigurable control law for AFTI/F-16 aircraft with failed right half elevator, has been designed for one flight condition using Porter's P1 control technique and responses are simulated including actuator and controller for G-command and pitch pointing maneuvers. The reconfigured control law achieved responses comparable to that of healthy aircraft except for the obvious fact that it requires more control surface deflections which are also within limits.
| Item Type: | Proj.Doc/Technical Report (Project Report) |
|---|---|
| Uncontrolled Keywords: | Flight control;Reconfigurable control;Multivariable control;Fault tolerance;Self repairing;Flight control; Damage tolerance |
| Subjects: | AERONAUTICS > Aircraft Stability and Control |
| Division/Department: | Aerospace Electronics and Controls Division |
| Depositing User: | Smt Bhagya Rekha KA |
| Date Deposited: | 17 Aug 2012 12:10 |
| Last Modified: | 17 Aug 2012 12:10 |
| URI: | http://nal-ir.nal.res.in/id/eprint/10795 |
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