Current methods of assessing flying qualities are based on linear system theory, which cannot capture the nonlinear phenomena commonly found at high angles of attack. Although bifurcation analysis has been proven to be a powerful tool for numerically analyzing nonlinear flight dynamics, in its standard (unforced) form, the method is unsuitable for flying qualities assessment as no information on the transient response is provided. To address this shortcoming, we propose the use of an extension of bifurcation analysis that treats the aircraft as a harmonically forced system. This facilitates the evaluation of the frequency-domain dynamics where the response is unsteady by definition. It is shown that the method can identify regions with strong nonlinearities that lead to degraded flying qualities. Time simulations of the closed-loop step responses in these undesirable regions show that despite the predictions of desirable behaviors using linear analysis, the closed-loop aircraft can still be attracted to an isola, experience control reversal, or have higher overshoot than anticipated.
|Title of host publication||AIAA Scitech 2021 Forum|
|Publisher||American Institute of Aeronautics and Astronautics Inc. (AIAA)|
|Publication status||Published - 4 Jan 2021|
|Event||2021 AIAA SciTech Forum - Virtual Event|
Duration: 4 Jan 2021 → 15 Jan 2021
|Conference||2021 AIAA SciTech Forum|
|Period||4/01/21 → 15/01/21|
Bibliographical noteprovisional acceptance date added, based on publication information.
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Nguyen, D. H., 2 Dec 2021
Student thesis: Doctoral Thesis › Doctor of Philosophy (PhD)File