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- W2070332555 abstract "Dynamic-inversion-based flight control laws present an attractive alternative to conventional gain-scheduled designs for high angle-of-attack maneuvering, where nonlinearities dominate the dynamics. Dynamic inversion is easily applied to the aircraft dynamics requiring a knowledge of the nonlinear equations of motion alone, rather than an extensive set of linearizations. However, the robustness properties of the dynamic inversion are questionable especially when considering the uncertainties involved with the aerodynamic database during post-stall flight. This paper presents a simple analysis and some preliminary results of simulations with a perturbed database. It is shown that incorporating integrators into the control loops helps to improve the performance in the presence of these perturbations." @default.
- W2070332555 created "2016-06-24" @default.
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- W2070332555 date "1992-08-10" @default.
- W2070332555 modified "2023-10-16" @default.
- W2070332555 title "Preliminary assessment of the robustness of dynamic inversion based flight control laws" @default.
- W2070332555 doi "https://doi.org/10.2514/6.1992-4330" @default.
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