標(biāo)題: Titlebook: Nonlinear Analysis and Synthesis Techniques for Aircraft Control; Declan Bates,Martin Hagstr?m Book 2007 Springer-Verlag Berlin Heidelberg [打印本頁] 作者: SORB 時間: 2025-3-21 16:23
書目名稱Nonlinear Analysis and Synthesis Techniques for Aircraft Control影響因子(影響力)
書目名稱Nonlinear Analysis and Synthesis Techniques for Aircraft Control影響因子(影響力)學(xué)科排名
書目名稱Nonlinear Analysis and Synthesis Techniques for Aircraft Control網(wǎng)絡(luò)公開度
書目名稱Nonlinear Analysis and Synthesis Techniques for Aircraft Control網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱Nonlinear Analysis and Synthesis Techniques for Aircraft Control被引頻次
書目名稱Nonlinear Analysis and Synthesis Techniques for Aircraft Control被引頻次學(xué)科排名
書目名稱Nonlinear Analysis and Synthesis Techniques for Aircraft Control年度引用
書目名稱Nonlinear Analysis and Synthesis Techniques for Aircraft Control年度引用學(xué)科排名
書目名稱Nonlinear Analysis and Synthesis Techniques for Aircraft Control讀者反饋
書目名稱Nonlinear Analysis and Synthesis Techniques for Aircraft Control讀者反饋學(xué)科排名
作者: IVORY 時間: 2025-3-21 22:26 作者: Armada 時間: 2025-3-22 02:25
Mikhail G. Goman,Andrew V. Khramtsovsky,Evgeny N. Kolesnikovdem Anf?nger leicht, geschniegelte Illustrationen zu malen, die sogar für wissenschaftliche Arbeiten und Fachbücher taugen. Der Wert der freih?ndig erreichbaren Sch?nheit und Genauigkeit liegt aber woanders: Der Zeichner gewinnt ein Stück Freiheit beim Nachdenken und Mitteilen wieder, das er sich, f作者: 幼兒 時間: 2025-3-22 07:10 作者: 馬賽克 時間: 2025-3-22 11:12
Jean-Marc Biannic,Andres Marcos,Declan G. Bates,Ian Postlethwaite作者: 使饑餓 時間: 2025-3-22 13:46
Clement Roos,Jean-Marc Biannic,Sophie Tarbouriech,Christophe Prieur作者: Carminative 時間: 2025-3-22 18:24
Prathyush P. Menon,Declan G. Bates,Ian Postlethwaite作者: 叫喊 時間: 2025-3-23 00:46
An LPV Control Law Design and Evaluation for the ADMIRE Modelcluding time and frequency domain criteria, linear and nonlinear simulation tests, and also piloted simulation in real time on the HELIFLIGHT simulator at the University of Liverpool. The performed evaluation clearly demonstrates that the designed LPV control laws satisfy most of the design requirem作者: FLUSH 時間: 2025-3-23 01:31 作者: organic-matrix 時間: 2025-3-23 09:08
John W. C. Robinsonueignen." (Maschinenmarkt)."Mit derartigen Methoden f?llt es auch dem Anf?nger leicht, geschniegelte Illustrationen zu malen, die sogar für wissenschaftliche Arbeiten und Fachbücher taugen. Der Wert der freih?ndig erreichbaren Sch?nheit und Genauigkeit liegt aber woanders: D978-3-642-24343-1作者: 谷物 時間: 2025-3-23 11:20
es auch dem Anf?nger leicht, geschniegelte Illustrationen zu malen, die sogar für wissenschaftliche Arbeiten und Fachbücher taugen. Der Wert der freih?ndig erreichbaren Sch?nheit und Genauigkeit liegt aber woanders: Der Zeichner gewinnt ein Stück Freiheit beim Nachdenken und Mitteilen wieder, das er sich, f978-3-642-02434-4作者: Erythropoietin 時間: 2025-3-23 15:11 作者: 法律的瑕疵 時間: 2025-3-23 20:19
978-3-540-73718-6Springer-Verlag Berlin Heidelberg 2007作者: probate 時間: 2025-3-24 01:31
Nonlinear Analysis and Synthesis Techniques for Aircraft Control978-3-540-73719-3Series ISSN 0170-8643 Series E-ISSN 1610-7411 作者: 叫喊 時間: 2025-3-24 04:50
The AIRBUS On-Ground Transport Aircraft Benchmarke main equations of motion. Loads affecting aircraft motion are then described and their modelling given. Finally a short aircraft behaviour analysis is provided. This chapter aims at offering the reader a clear understanding of the control application and its requirements.作者: 驚奇 時間: 2025-3-24 08:23 作者: AIL 時間: 2025-3-24 12:48
Lecture Notes in Control and Information Scienceshttp://image.papertrans.cn/n/image/667326.jpg作者: 愚笨 時間: 2025-3-24 18:23 作者: 碌碌之人 時間: 2025-3-24 20:40 作者: FEAT 時間: 2025-3-24 23:32 作者: 內(nèi)閣 時間: 2025-3-25 06:51 作者: Tincture 時間: 2025-3-25 09:07 作者: disparage 時間: 2025-3-25 11:44
Nonlinear Symbolic LFT Tools for Modelling, Analysis and Designbines the natural modularity and clarity of presentation from LFT modelling with the ease of manipulation from symbolic algebra. It results in an exact nonlinear symbolic LFT that represents an ideal starting point to apply subsequent assumptions and simplifications to finally transform the model in作者: 態(tài)學(xué) 時間: 2025-3-25 15:59
Nonlinear LFT Modelling for On-Ground Transport Aircraftdentification approach and a general nonlinear symbolic LFT modelling framework. It is shown how the modelling framework is applicable to derive an exact LFT model of the aircraft-on-ground as well as some simplified design-oriented versions. An important contribution is the proposed force identific作者: conference 時間: 2025-3-25 21:49 作者: 說不出 時間: 2025-3-26 01:25
Rapid Prototyping Using Inversion-Based Control and Object-Oriented Modelling modelling approach allows for automatic generation of regular, static, as well as inverse simulation models. Inverse models form the basis of various commonly used nonlinear controller synthesis methods, such as Feedback Linearisation. The resulting multivariable control laws are easily tuned to me作者: Hemiplegia 時間: 2025-3-26 05:50 作者: armistice 時間: 2025-3-26 11:05
An LPV Control Law Design and Evaluation for the ADMIRE Modeltransonic and supersonic regions. The design of the LPV control law is based on the parameter-dependent Lyapunov function approach with gridding of the parameter space. It is demonstrated that by using a linear piece-wise interpolation of the aircraft model the LPV approach allows the design of a co作者: TIGER 時間: 2025-3-26 12:45 作者: Pigeon 時間: 2025-3-26 19:36 作者: 脫離 時間: 2025-3-26 23:26
Investigation of the ADMIRE Manoeuvring Capabilities Using Qualitative Methodss, local stability maps and two-dimensional cross-sections of stability regions for stable equilibria considering the velocity-vector roll manoeuvre. A nonlinear dynamic inversion control law is implemented as a prototype of a control and stability augmentation system. The analysis of the closed-loo作者: Blasphemy 時間: 2025-3-27 02:45 作者: Reverie 時間: 2025-3-27 06:12
Concluding Remarksin aerospace vehicles. To guarantee the industrial relevance of the project, two highly realistic simulation models were developed, together with demanding design/analysis challenges. These benchmarks in themselves represent significant achievements of the project, since there are still very few ind作者: 沉默 時間: 2025-3-27 11:25
Maria E. Sidoryuk,Mikhail G. Goman,Stephen Kendrick,Daniel J. Walker,Philip Perfect Berufsschulen werden die einfachen Zeichentechniken unterrichtet und geübt. Der Leser dieses Lehrbuches erlebt, wie er technische Formen, Zusammenh?nge und Ideen zeitsparend und überzeugend darstellen kann. Viele Beispiele und praktische übungen führen ihn in kurzer Zeit zu professionellen Handzeic作者: 原始 時間: 2025-3-27 14:15 作者: 你正派 時間: 2025-3-27 19:12 作者: relieve 時間: 2025-3-28 00:25
aterial: .Durch den zunehmenden Einsatz von 3D-CAD-Systemen erlangt das technische Freihandzeichnen eine neue Bedeutung. Der Leser dieses praxisbew?hrten Buches erf?hrt, wie er technische Formen, Zusammenh?nge und Ideen zeitsparend und überzeugend darstellen kann. Das schrittweise Vorgehen, die Disk作者: Visual-Acuity 時間: 2025-3-28 04:50 作者: 要塞 時間: 2025-3-28 09:11 作者: legitimate 時間: 2025-3-28 12:21
On-Ground Transport Aircraft Nonlinear Control Design and Analysis Challengess. The control objectives may also vary depending on the rolling phase: taxiing, runway acceleration prior to take-off, runway deceleration after landing, and runway deceleration after a rejected take-off.作者: Pathogen 時間: 2025-3-28 18:09 作者: GEAR 時間: 2025-3-28 19:19 作者: goodwill 時間: 2025-3-29 00:24 作者: 彩色的蠟筆 時間: 2025-3-29 06:54
Nonlinear LFT Modelling for On-Ground Transport Aircraft a reduced-order LFT plant where the Δ block only contains time-varying or constant (but uncertain) parameters on the one hand, and saturation-type non-linearities on the other hand. Such a model is then very useful for applying modern analysis and synthesis techniques.作者: 小教堂 時間: 2025-3-29 07:20 作者: 全國性 時間: 2025-3-29 12:05
Investigation of the ADMIRE Manoeuvring Capabilities Using Qualitative Methods between control inputs helps to avoid control surfaces saturation and to significantly enhance the ADMIRE manoeuvrability at high angles of attack. A number of computational examples for attainable equilibrium sets and regions of attraction illustrate the applied investigation methodology.作者: 清洗 時間: 2025-3-29 18:59 作者: Charitable 時間: 2025-3-29 21:55
Robustness Analysis Versus Mixed LTI/LTV Uncertainties for On-Ground Aircrafts then introduced to solve the problem. The application of this method to the on-ground aircraft finally reveals the good robustness properties of the lateral controller despite uncertainties and saturation effects. It also gives some relevant information that enables further improvements to be made to the design.作者: 下邊深陷 時間: 2025-3-30 03:37 作者: hereditary 時間: 2025-3-30 07:24 作者: 辭職 時間: 2025-3-30 10:05
9樓作者: 廣告 時間: 2025-3-30 14:39
9樓作者: 危險 時間: 2025-3-30 20:01
10樓作者: B-cell 時間: 2025-3-30 21:59
10樓作者: BRAVE 時間: 2025-3-31 01:33
10樓作者: 爆米花 時間: 2025-3-31 06:48
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