2020
DOI: 10.2514/1.g004303
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Multiple-Timescale Nonlinear Control of Aircraft with Model Uncertainties

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Cited by 9 publications
(3 citation statements)
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“…where f e ξ , f eη , and f e ϕ are defined such that ( 17) and ( 18) are identitically equal to the vector field in (16). This last representation obscures the timescale behavior because O(f e ϕ ) ̸ = O(1).…”
Section: A Augmented Error Dynamicsmentioning
confidence: 99%
See 1 more Smart Citation
“…where f e ξ , f eη , and f e ϕ are defined such that ( 17) and ( 18) are identitically equal to the vector field in (16). This last representation obscures the timescale behavior because O(f e ϕ ) ̸ = O(1).…”
Section: A Augmented Error Dynamicsmentioning
confidence: 99%
“…However, adaptive control has yet to be considered by multipletimescale control researchers. Saha and Valasek designed controllers for uncertain singularly perturbed plants [13], [14], [15], [16], but their method derives the adaption laws using a full-order Lyapunov analysis. This makes their method difficult to generalize.…”
Section: Introductionmentioning
confidence: 99%
“…Dynamic Inversion (NDI) is a nonlinear feedback linearization technique that has been widely applied to flight control systems [1,2]. Using state feedback and the inverted nonlinear system dynamics, NDI can significantly reduce controller development costs by avoiding gain scheduling and Jacobian linearization at a multitude of operating points.…”
mentioning
confidence: 99%