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Results 1 to 25 of 178

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Effect of Microtab on Reduction of Noise Due to Aircraft High-Lift DevicesKUO, Brian C; SARIGUL-KLIJN, Nesrin.Journal of aircraft. 2009, Vol 46, Num 5, pp 1812-1815, issn 0021-8669, 4 p.Article

Pilot-Involved-Oscillation Suppression Using Low-Order Antiwindup: Flight-Test EvaluationBRIEGER, Oliver; KERR, Murray; POSTLETHWAITE, Ian et al.Journal of guidance, control, and dynamics. 2012, Vol 35, Num 2, pp 471-483, issn 0731-5090, 13 p.Article

Adaptive control for a nonlinear wing section with multiple flapsBEHAL, A; RAE, V. M; MARZOCCA, P et al.Journal of guidance, control, and dynamics. 2006, Vol 29, Num 3, pp 744-749, issn 0731-5090, 6 p.Article

Robust Aeroelastic Control of Lifting Surfaces with Uncertainty via Multi-Objective SynthesisNA, Sungsoo; JEONG, In-Joo; YOON, Gwon-Chan et al.Journal of guidance, control, and dynamics. 2009, Vol 32, Num 1, pp 337-343, issn 0731-5090, 7 p.Article

Bifurcation Analysis of Aircraft with Structural Nonlinearity and Freeplay Using Numerical ContinuationDIMITRIADIS, G.Journal of aircraft. 2008, Vol 45, Num 3, pp 893-905, issn 0021-8669, 13 p.Article

Trial Input Method and Own-Aircraft State Prediction in Autonomous Air CombatYIQUN DONG; JIANLIANG AI.Journal of aircraft. 2012, Vol 49, Num 3, pp 947-954, issn 0021-8669, 8 p.Article

Latching Control of an Oscillating Water Column Spar-Buoy Wave Energy Converter in Regular WavesHENRIQUES, J. C. C; FALCAO, A. F. O; GOMES, R. P. F et al.Journal of offshore mechanics and Arctic engineering. 2013, Vol 135, Num 2, issn 0892-7219, 021902.1-021902.8Article

A high-rate shape memory alloy actuator for aerodynamic load control on wind turbinesLARA-QUINTANILLA, Adrian; HULSKAMP, Anton W; BERSEE, Harald E. N et al.Journal of intelligent material systems and structures. 2013, Vol 24, Num 15, pp 1834-1845, issn 1045-389X, 12 p.Article

Detection of faults in flight control actuators with hard saturation and friction non-linearityMADHAVANPILLAI, Jayakumar; DAS, Bijan B.International journal of reliability and safety (Print). 2013, Vol 7, Num 2, pp 108-127, issn 1479-389X, 20 p.Article

Composite Control Strategy of Stratospheric Airships with Moving MassesCHEN, L; ZHOU, G; YAN, X. J et al.Journal of aircraft. 2012, Vol 49, Num 3, pp 794-801, issn 0021-8669, 8 p.Article

Hybrid Fault-Tolerant Flight Control System Design Against Partial Actuator FailuresXIANG YU; JIN JIANG.IEEE transactions on control systems technology. 2012, Vol 20, Num 4, pp 871-886, issn 1063-6536, 16 p.Article

Numerical simulation of flapping wings using a panel method and a high-order Navier―Stokes solverPERSSON, P.-O; WILLIS, D. J; PERAIRE, J et al.International journal for numerical methods in engineering. 2012, Vol 89, Num 10, pp 1296-1316, issn 0029-5981, 21 p.Article

Evolving a Multiagent Controller for Micro Aerial VehiclesSALICHON, Max; TURNER, Kagan.IEEE transactions on systems, man and cybernetics. Part C, Applications and reviews. 2012, Vol 42, Num 6, pp 1772-1783, issn 1094-6977, 12 p.Article

Adaptive control of a nonlinear aeroelastic systemDAOCHUN LI; JINWU XIANG; SHIJUN GUO et al.Aerospace science and technology (Imprimé). 2011, Vol 15, Num 5, pp 343-352, issn 1270-9638, 10 p.Article

Flight Dynamics and Stability of a Tethered Inflatable KiteplaneTERINK, E. J; BREUKELS, J; SCHMEHL, R et al.Journal of aircraft. 2011, Vol 48, Num 2, pp 503-513, issn 0021-8669, 11 p.Article

Shooting-Based Complete Bifurcation Prediction for Aeroelastic Systems with FreeplayDIMITRIADIS, Grigorios.Journal of aircraft. 2011, Vol 48, Num 6, pp 1864-1877, issn 0021-8669, 14 p.Article

Design, analysis and experimental validation of a morphing UAV wingBOLINCHES, M; KEANE, A. J; FORRESTER, A. I. J et al.Aeronautical Journal. 2011, Vol 115, Num 1174, pp 761-765, issn 0001-9240, 5 p.Conference Paper

Helicopter blade flapping with and without small angle assumption in the presence of dynamic stallJYOTI RANJAN MAJHI; GANGULI, Ranjan.Applied mathematical modelling. 2010, Vol 34, Num 12, pp 3726-3740, issn 0307-904X, 15 p.Article

Performing co-ordinated turns with articulated wing-tips as multi-axis control effectorsBOURDIN, P; GATTO, A; FRISWELL, M. I et al.Aeronautical Journal. 2010, Vol 114, Num 1151, pp 35-47, issn 0001-9240, 13 p.Article

Prediction and Analysis of Main Rotor Loads in a Prescribed Pull-Up ManeuverABHISHEK, A; DATTA, Anubhav; ANANTHAN, Shreyas et al.Journal of aircraft. 2010, Vol 47, Num 4, pp 1197-1215, issn 0021-8669, 19 p.Article

Load Alleviation on a Joined-Wing Unmanned AircraftPALETTA, Nicola; BELARDO, Marika; PECORA, Modesto et al.Journal of aircraft. 2010, Vol 47, Num 6, pp 2005-2016, issn 0021-8669, 12 p.Article

Attitude Guidance for Spinning Vehicles with Independent Pitch and Yaw ControlCREAGH, Michael A; MEET, David J.Journal of guidance, control, and dynamics. 2010, Vol 33, Num 3, pp 915-922, issn 0731-5090, 8 p.Conference Paper

Development & Flight Test of a Shape Memory Alloy Actuator Flight Control SystemBRENNISON, M; BARRETT, R. M; KERTH, L et al.Proceedings of SPIE, the International Society for Optical Engineering. 2010, Vol 7643, issn 0277-786X, isbn 978-0-8194-8058-3, 764334.1-764334.14, 2Conference Paper

Dynamics and autopilot design for endoatmospheric interceptors with dual control systemsDI ZHOU; CHUNTAO SHAO.Aerospace science and technology (Imprimé). 2009, Vol 13, Num 6, pp 291-300, issn 1270-9638, 10 p.Article

Modal Transformation Method for Deformable Membrane MirrorsSHEPHERD, Michael J; COBB, Richard G; PALAZOTTO, Anthony N et al.Journal of guidance, control, and dynamics. 2009, Vol 32, Num 1, pp 276-289, issn 0731-5090, 14 p.Article

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