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Titlebook: Modern Aircraft Flight Control; Miomir Vukobratovi?,Radoslav Stoji? Book 1988 Springer-Verlag Berlin Heidelberg 1988 Tracking.control.mode

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發(fā)表于 2025-3-21 19:41:45 | 只看該作者 |倒序瀏覽 |閱讀模式
書目名稱Modern Aircraft Flight Control
編輯Miomir Vukobratovi?,Radoslav Stoji?
視頻videohttp://file.papertrans.cn/637/636900/636900.mp4
叢書名稱Lecture Notes in Control and Information Sciences
圖書封面Titlebook: Modern Aircraft Flight Control;  Miomir Vukobratovi?,Radoslav Stoji? Book 1988 Springer-Verlag Berlin Heidelberg 1988 Tracking.control.mode
描述A complete dynamic model of flight dynamics is presented. Based on this model, the inverse problem and that of the synthesis of programmed motion are solved. A new approach to decoupled control of large-scale nonlinear systems is applied to dynamic flight control. Control synthesis is performed in two steps. First the nominal programmed control is synthesized using the complete model of flight dynamics. This nominal control should realize nominal trajectory under ideal conditions with no perturbations. At the second step the tracking of nominal trajectory is realized. The system is viewed as a set of decoupled subsystems and for each subsystem local control is synthesized. Then the stability of the overall system is analyzed and global control is introduced to compensate coupling among some of the subsystems. In the book a particular choice of subsystems is proposed in a case of flight control, and the local and global control synthesis is presented. Extensive simulations of flight control with different control laws are also presented.
出版日期Book 1988
關(guān)鍵詞Tracking; control; model; nonlinear system; simulation; stability; stabilization
版次1
doihttps://doi.org/10.1007/BFb0043099
isbn_softcover978-3-540-19119-3
isbn_ebook978-3-540-39122-7Series ISSN 0170-8643 Series E-ISSN 1610-7411
issn_series 0170-8643
copyrightSpringer-Verlag Berlin Heidelberg 1988
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發(fā)表于 2025-3-21 22:30:50 | 只看該作者
Book 1988solved. A new approach to decoupled control of large-scale nonlinear systems is applied to dynamic flight control. Control synthesis is performed in two steps. First the nominal programmed control is synthesized using the complete model of flight dynamics. This nominal control should realize nominal
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0170-8643 f flight control, and the local and global control synthesis is presented. Extensive simulations of flight control with different control laws are also presented.978-3-540-19119-3978-3-540-39122-7Series ISSN 0170-8643 Series E-ISSN 1610-7411
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Lecture Notes in Control and Information Scienceshttp://image.papertrans.cn/m/image/636900.jpg
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Krein Signature in Hamiltonian and ,-Symmetric Systems,for the onset of instability past the bifurcation point requires existence of two simple neutrally stable eigenvalues of opposite Krein signatures before the bifurcation point. This property is useful in the parameter continuations of neutrally stable eigenvalues of the linearized Gross–Pitaevskii equation.
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,Customer confusion in Service-to-Business Markets — Foundations and First Empirical Results,wever, as seen in the example of outsourcing solutions, blatant inefficiencies exist in purchase decision-making: 80% of business process outsourcing contracts have to be renegotiated within two years, and 20% of these renegotiated contracts fail (.; .; .; .). How can the high failure-rate in the pu
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