Handling Quality-Oriented Tuning Procedure of a Dynamic Inversion Control Law via a Robust Control Technique

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dc.contributor.authorResit, Demirkiran
dc.contributor.authorHasan, Isci
dc.contributor.authorErcument, Turkoglu
dc.date.accessioned2025-03-17T12:27:48Z
dc.date.available2025-03-17T12:27:48Z
dc.date.issued2024
dc.departmentTarsus Üniversitesi
dc.descriptionAIAA SciTech Forum -- JAN 08-12, 2024--AG289 Orlando, FL
dc.description.abstractThe robustness of a flight control law has played an important role. Designers can achieve this objective by using different techniques; however, if the target platform has a wide range of the flight envelope and desired behavior is demanding (e.g., fighter aircraft), completing a robust design becomes a challenging task while requested high performance capability. Using both the dynamic inversion philosophy and robust control design methodology can be a good choice in terms of meeting the essential requirements of flight control law design. Enhancing the handling qualities while not losing robustness is a common trade-off in the classic a flight control law development process. In order to improve the handling quality, tuning the feed-forward term instead of feedback terms is a valuable approach to preserve the robustness of the closed loops. Tuning procedure according to the proposed idea is explained in detail throughout the paper. The control design steps and the results of comprehensive set of stability, robustness and handling qualities by considering the proposed flight control law with additional terms are addressed. Besides, the achieved entire results indicate that the requirements of stability, handling qualities, and robustness is met by offered control law development strategies.
dc.description.sponsorshipAIAA
dc.identifier.isbn978-1-62410-711-5
dc.identifier.scopus2-s2.0-85198621611
dc.identifier.scopusqualityN/A
dc.identifier.urihttps://hdl.handle.net/20.500.13099/2456
dc.identifier.wosWOS:001375995202022
dc.identifier.wosqualityN/A
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherAmer Inst Aeronautics & Astronautics
dc.relation.ispartofAiaa Scitech 2024 Forum
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.snmzKA_WOS_20250316
dc.subjectFlight
dc.subjectStability
dc.subjectDesign
dc.titleHandling Quality-Oriented Tuning Procedure of a Dynamic Inversion Control Law via a Robust Control Technique
dc.typeConference Object

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