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Titlebook: Nonlinear Control of Fixed-Wing UAVs with Time-Varying and Unstructured Uncertainties; Michail G. Michailidis,Kimon P. Valavanis,Matthew

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發(fā)表于 2025-3-21 16:30:51 | 只看該作者 |倒序瀏覽 |閱讀模式
書目名稱Nonlinear Control of Fixed-Wing UAVs with Time-Varying and Unstructured Uncertainties
編輯Michail G. Michailidis,Kimon P. Valavanis,Matthew
視頻videohttp://file.papertrans.cn/668/667377/667377.mp4
概述Presents recent research on nonlinear control of fixed-wing unmanned aerial vehicles with time-varying and unstructured uncertainties.Describes techniques that can be generalized and applied to next-g
叢書名稱Springer Tracts in Autonomous Systems
圖書封面Titlebook: Nonlinear Control of Fixed-Wing UAVs with Time-Varying and Unstructured Uncertainties;  Michail G. Michailidis,Kimon P. Valavanis,Matthew
描述This book introduces a comprehensive and mathematically rigorous controller design for families of nonlinear systems with time-varying parameters and unstructured uncertainties. Although the presented methodology is general, the specific family of systems considered is the latest, NextGen, unconventional fixed-wing unmanned aircraft with circulation control or morphing wings, or a combination of both..The approach considers various sources of model and parameter uncertainty, while the controller design depends not on a nominal plant model, but instead on a family of admissible plants. In contrast to existing controller designs that consider multiple models and multiple controllers, the proposed approach is based on the ‘one controller fits all models’ within the unstructured uncertainty interval..The book presents a modeling-based analysis and synthesis approach with additive uncertainty weighting functions for accurate realization of the candidate systems. This differs significantly from existing designs in that it is capable of handling time-varying characteristics.??.This research monograph is suitable for scientists, engineers, researchers and graduate students with a backgroun
出版日期Book 2020
關(guān)鍵詞Autonomous Systems; UAV; Unmanned Aerial vehicles; Nonlinear Control; Robust Control
版次1
doihttps://doi.org/10.1007/978-3-030-40716-2
isbn_softcover978-3-030-40718-6
isbn_ebook978-3-030-40716-2Series ISSN 2662-5539 Series E-ISSN 2662-5547
issn_series 2662-5539
copyrightSpringer Nature Switzerland AG 2020
The information of publication is updating

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發(fā)表于 2025-3-21 23:47:19 | 只看該作者
Michail G. Michailidis,Kimon P. Valavanis,Matthew J. Rutherfords professor from Teachers College, Columbia University and Senior Scholar at the Carnegie Foundation for the Advancement of Teaching...."Mary Kooy is a gifted writer and teacher. She takes the obvious truth that we read books with other people and turns it into a compelling work of professional deve
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發(fā)表于 2025-3-22 09:57:51 | 只看該作者
Foundation for the Advancement of Teaching...."Mary Kooy is a gifted writer and teacher. She takes the obvious truth that we read books with other people and turns it into a compelling work of professional deve978-1-4419-4158-9978-0-387-33927-6
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發(fā)表于 2025-3-22 16:33:28 | 只看該作者
Michail G. Michailidis,Kimon P. Valavanis,Matthew J. RutherfordFoundation for the Advancement of Teaching...."Mary Kooy is a gifted writer and teacher. She takes the obvious truth that we read books with other people and turns it into a compelling work of professional deve978-1-4419-4158-9978-0-387-33927-6
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發(fā)表于 2025-3-22 18:17:23 | 只看該作者
Michail G. Michailidis,Kimon P. Valavanis,Matthew J. RutherfordFoundation for the Advancement of Teaching...."Mary Kooy is a gifted writer and teacher. She takes the obvious truth that we read books with other people and turns it into a compelling work of professional deve978-1-4419-4158-9978-0-387-33927-6
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發(fā)表于 2025-3-23 00:29:13 | 只看該作者
2662-5539 ficantly from existing designs in that it is capable of handling time-varying characteristics.??.This research monograph is suitable for scientists, engineers, researchers and graduate students with a backgroun978-3-030-40718-6978-3-030-40716-2Series ISSN 2662-5539 Series E-ISSN 2662-5547
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發(fā)表于 2025-3-23 04:11:58 | 只看該作者
Case Study,ifferent . flight dynamics. Therefore, the actual . flight dynamics are explicitly described by a family of models or by model uncertainty mainly stemming from the aerodynamic coefficients, with predefined upper and lower bounds.
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