Robust Flight Control Design to Minimize Aircraft Loss-of-Control Incidents
A pseudo-sliding mode control synthesis procedure discussed previously in the literature is applied to the design of a control system for a nonlinear model of the NASA Langley Generic Transport Model. The complete vehicle model is included as an appendix. The goal of the design effort is the synthes...
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| Format: | Article |
| Language: | English |
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MDPI AG
2013-11-01
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| Series: | Aerospace |
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| Online Access: | http://www.mdpi.com/2226-4310/1/1/1 |