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Titlebook: Advances in Aerospace Guidance, Navigation and Control; Selected Papers of t Florian Holzapfel,Stephan Theil Conference proceedings 2011 Sp

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發(fā)表于 2025-3-21 19:39:47 | 只看該作者 |倒序瀏覽 |閱讀模式
期刊全稱Advances in Aerospace Guidance, Navigation and Control
期刊簡稱Selected Papers of t
影響因子2023Florian Holzapfel,Stephan Theil
視頻videohttp://file.papertrans.cn/147/146629/146629.mp4
發(fā)行地址State of the art of Aerospace Guidance, Navigation and Control.Presents the selected papers of the 1st CEAS Specialist Conference on Guidance, Navigation and Control held in Munich, Germany, April 13t
圖書封面Titlebook: Advances in Aerospace Guidance, Navigation and Control; Selected Papers of t Florian Holzapfel,Stephan Theil Conference proceedings 2011 Sp
影響因子.Over the last few decades, both the aeronautics and space disciplines have greatly influenced advances in controls, sensors, data fusion and navigation. Many of those achievements that made the word “aerospace” synonymous with “high–tech” were enabled by innovations in guidance, navigation and control..?.Europe has seen a strong trans-national consolidation process in aerospace over the last few decades. Most of the visible products, like commercial aircraft, fighters, helicopters, satellites, launchers or missiles, are not made by a single country – they are the fruits of cooperation. No European country by itself hosts a specialized guidance, navigation and controls community large enough to cover the whole spectrum of disciplines. However, on a European scale, mutual exchange of ideas, concepts and solutions is enriching for all. The 1st CEAS Specialist Conference on Guidance, Navigation and Control is an attempt to bring this community together..?.This book is a selection of papers presented at the conference. All submitted papers have gone through a formal review process in compliance with good journal practices. The best papers have been recommended by the reviewers to be pu
Pindex Conference proceedings 2011
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Pertti Hari,Eero Nikinmaa,Markku Kulmalae engines activity and reduction of robustness properties. Another goal is to keep the control law and its tuning as simple as possible: for this a control law structure whose terms can easily be interpreted is proposed. The capability of the proposed control law to permit safe landing was shown by simulator tests as well as flight tests.
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發(fā)表于 2025-3-22 05:57:08 | 只看該作者
,Halbleiter für Bordnetzanwendungen,rithm presented is used in the gain design process of the lateral part of the flight control system for a generic transport aircraft. Results obtained with this novel approach are analyzed regarding the SISO and MIMO stability margins.
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,Einführung Bordnetzstrukturen,ncertainties (e.g. aircraft mass) as well as low friction coefficients at the interface tyre-ground. In order to test the tracking controller, an accurate virtual aircraft model has been designed in Modelica, with particular attention to the landing gears.
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Boreal Forest and Climate Change projection of predicted path angle on a surface sliding in the tunnel and located on appropriately selected distance ahead. The results demonstrated that the developed technique allowed considerable improving accuracy in each piloting task.
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