Attitude Controller for UAV First-Order Acceleration Coefficients Tracking. [PDF]
Sensors (Basel)Xu D, Pei H.
europepmc +1 more source
Certified Reductions of the Weight-6 Euler Sum S₄,₂(x) at Dyadic Arguments
Keenan Williams
openalex +1 more source
Contour Integrations and Parity Results of Cyclotomic Euler $T$-Sums and Multiple $t$-Values [PDF]
Zhenlu Wang, Ce Xu
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Optimal Homogeneous ℒp$$ {\boldsymbol{\mathcal{L}}}_{\boldsymbol{p}} $$‐Gain Controller
International Journal of Robust and Nonlinear Control, EarlyView.ABSTRACT Nonlinear ℋ∞$$ {\mathscr{H}}_{\infty } $$‐controllers are designed for arbitrarily weighted, continuous homogeneous systems with a focus on systems affine in the control input. Based on the homogeneous ℒp$$ {\mathcal{L}}_p $$‐norm, the input–output behavior is quantified in terms of the homogeneous ℒp$$ {\mathcal{L}}_p $$‐gain as a ...
Daipeng Zhang +3 more
wiley +1 more source
The increased drift of steep focusing surface gravity waves. [PDF]
J Fluid MechBlaser A, Lenain L, Pizzo N.
europepmc +1 more source
Contour Integrations and Parity Results of Cyclotomic Euler Sums and Multiple Polylogarithm Function [PDF]
Rui, Hongyuan, C. J. Xu
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Optimal Gain Selection for the Arbitrary‐Order Homogeneous Differentiator
International Journal of Robust and Nonlinear Control, EarlyView.ABSTRACT Differentiation of noisy signals is a relevant and challenging task. Widespread approaches are the linear high‐gain observer acting as a differentiator and Levant's robust exact differentiator with a discontinuous right‐hand side. We consider the family of arbitrary‐order homogeneous differentiators, which includes these special cases.
Benjamin Calmbach +2 more
wiley +1 more source
An Unscented Kalman Filter Based on the Adams-Bashforth Method with Applications to the State Estimation of Osprey-Type Drones Composed of Tiltable Rotor Mechanisms. [PDF]
Sensors (Basel)Watanabe K, Takeda S, Nagai I.
europepmc +1 more source
Iteration Sums of The Euler Totient Function Regarding Powers of Fermat Primes [PDF]
Li, Xiang, Allison M. Pacelli
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Sliding Mode Control in Aerospace Applications: A Survey
International Journal of Robust and Nonlinear Control, EarlyView.ABSTRACT Sliding mode control (SMC) enjoys robustness to matched and unmatched (in the case of minimum phase input‐output dynamics) bounded perturbations, and finite time convergence. Second‐order and higher‐order sliding mode control systems (2‐SMC/HOSMC) retain all the advantages of sliding mode control, but in addition can be applied to systems of ...
Yuri Shtessel, Christopher Edwards
wiley +1 more source