Santharam, A (1988) Model Following control for a Light Combat Aircraft. Project Report. NAL, Bangalore.
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Abstract
The design of a candidate control law for LCA to improve longitudinal handling quality by satisfying C* criteria which is a blend of normal acceleration and pitch rate is . addressed The model following control technic used, wherein the pilot input goes through a dynamic C* model and feed forward gains so that the C* of aircraft is forced to follow that of the model in addition to satisfying short period damping and natural frequency requirements . The perfect model following, optimal model following and pole placement technics are used for computing feed back and feed forward gains .
| Item Type: | Proj.Doc/Technical Report (Project Report) |
|---|---|
| Uncontrolled Keywords: | Model Following;Optimal Control;Handling Quality;Active Controls;Control Configured Vehicle |
| Subjects: | AERONAUTICS > Aircraft Design, Testing & Performance AERONAUTICS > Aircraft Stability and Control |
| Division/Department: | Aerospace Electronics and Controls Division |
| Depositing User: | Mr Nisanth |
| Date Deposited: | 16 Jul 2012 11:43 |
| Last Modified: | 16 Jul 2012 11:43 |
| URI: | http://nal-ir.nal.res.in/id/eprint/10575 |
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