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Variable structure robust flight control system for the F-14 |
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| Authors: | Singh SN Steinberg M DiGirolamo RD |
| Institution: | Nevada Univ., Las Vegas, NV, USA; |
| Abstract: | In this paper, a flight control law for a simplified F-14 aircraft model is designed based on variable structure control (VSC) theory. For m-input, q-output linear uncertain systems (q |
| Keywords: | |