Works matching DE "AIRPLANE control systems"
Results: 161
Can intention override the “automatic pilot”?
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- Experimental Brain Research, 2010, v. 202, n. 3, p. 623, doi. 10.1007/s00221-010-2169-7
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Curvilinear Approach to Landing.
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- Transactions on Aerospace Research, 2024, v. 2024, n. 1, p. 1, doi. 10.2478/tar-2024-0001
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H∞ Preview Control for Automatic Carrier Landing.
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- Transactions of Nanjing University of Aeronautics & Astronautics, 2019, v. 36, n. 6, p. 919, doi. 10.16356/j.1005-1120.2019.06.005
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Multiagent Control of Airplane Wing Stability with "Feathers" under the Flexural Torsional Flutter.
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- Mathematics (2227-7390), 2022, v. 10, n. 2, p. 236, doi. 10.3390/math10020236
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飞机舵面缝隙缺陷建模及电磁散射特性分析.
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- Telecommunication Engineering, 2022, v. 62, n. 3, p. 336, doi. 10.3969/j.issn.1001-893x.2022.03.010
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Technological Change from Analog to Digital: Aircraft Engine Control System.
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- Annals of Business Administrative Science (ABAS), 2014, v. 13, n. 6, p. 329, doi. 10.7880/abas.13.329
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Genetic algorithm design of type-1 and type-2 fuzzy logic systems for airplane control.
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- Mathematics in Engineering, Science & Aerospace (MESA), 2014, v. 5, n. 1, p. 1
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Hybrid tracking control of fixed wing aerial vehicles.
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- Mathematics in Engineering, Science & Aerospace (MESA), 2011, v. 2, n. 4, p. 371
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Analysis of Loss of Control Parameters for Aircraft Maneuvering in General Aviation.
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- Journal of Advanced Transportation, 2018, p. 1, doi. 10.1155/2018/7865362
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UÇUŞ KONTROL SİSTEMİNDE GÖZLEYİCİ KULLANARAK ARIZA TESPİTİ.
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- Journal of Aeronautics & Space Technologies / Havacilik ve Uzay Teknolojileri Dergisi, 2006, v. 2, n. 4, p. 15
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BİR UÇAĞIN İRTİFA KONTROLÜNDE KLASİK VE BULANIK PD DENETLEYİCİ PERFORMANSLARININ KARŞILAŞTIRILMASI.
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- Journal of Aeronautics & Space Technologies / Havacilik ve Uzay Teknolojileri Dergisi, 2006, v. 2, n. 3, p. 9
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On 'Living in a Box': Distributed Control and Automation Surprises.
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- Technikgeschichte, 2020, v. 87, n. 1, p. 43, doi. 10.5771/0040-117X-2020-1-43
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HUMAN FACTORS ANALYSIS OF ACCIDENTS IN SYSTEM OF SYSTEMS.
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- Journal of Battlefield Technology, 2012, v. 15, n. 2, p. 23
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NECESSARY AND SUFFICIENT CONDITIONS FOR THE WELL-POSEDNESS OF A BOUNDARY VALUE PROBLEM FOR A LINEAR LOADED HYPERBOLIC EQUATION.
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- Journal of Mathematics, Mechanics & Computer Science, 2021, v. 112, n. 4, p. 3, doi. 10.26577/JMMCS.2021.v112.i4.01
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Coordinated target assignment via a finite-time gain measurement approach.
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- IET Control Theory & Applications (Wiley-Blackwell), 2013, v. 7, n. 3, p. 343, doi. 10.1049/iet-cta.2011.0212
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The necessity of introducing a geometric control subsystem into the composite attitude control systems of spacecraft and aircraft with modern precision.
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- Doklady Physics, 2016, v. 61, n. 1, p. 5, doi. 10.1134/S1028335816010079
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CUDA-BASED TECHNOLOGY FOR IMPROVING THE EFFICIENCY OF THE AIRCRAFT MOTION.
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- Electronics & Control Systems, 2016, v. 4, n. 50, p. 58, doi. 10.18372/1990-5548.50.11388
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SYNTHESIS ALGORITHM OF THE MOVING PLANT CONTROL SIGNALS OBSERVER.
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- Electronics & Control Systems, 2016, v. 49, n. 3, p. 22
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DESIGN OF ROBUST CONTROLLER FOR UAV INFORMATION-MEASURING DEVICES STABILIZATION SYSTEM.
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- Electronics & Control Systems, 2013, v. 3, n. 37, p. 58
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FLIGHT CONTROL SYSTEM DESIGN VIA LMI-APPROACH.
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- Electronics & Control Systems, 2013, v. 3, n. 37, p. 49
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Application of Multidisciplinary Systems-of-Systems Optimization to an Aircraft Design Problem.
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- Systems Engineering, 2016, v. 19, n. 3, p. 235, doi. 10.1002/sys.21358
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Minimum energy oriented global stabilizing control of the PVTOL aircraft.
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- International Journal of Control, 2007, v. 80, n. 3, p. 430, doi. 10.1080/00207170601069505
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APPLICATION THE GPS OBSERVATIONS IN SPP METHOD FOR AIRCRAFT POSITIONING IN FLIGHT EXPERIMENT IN DĘBLIN, POLAND (01.06.2010).
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- Journal of Automation, Mobile Robotics & Intelligent Systems, 2017, v. 11, n. 1, p. 42, doi. 10.14313/JAMRIS_1-2017/5
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Designing a Control System for an Airplane Wing Flutter Employing Gas Actuators.
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- International Journal of Aerospace Engineering, 2017, p. 1, doi. 10.1155/2017/4209619
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Three-Dimensional Integrated Guidance and Control for Near Space Interceptor Based on Robust Adaptive Backstepping Approach.
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- International Journal of Aerospace Engineering, 2016, p. 1, doi. 10.1155/2016/6598983
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Research on Aircraft Attack Angle Control Considering Servo-Loop Dynamics.
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- International Journal of Aerospace Engineering, 2015, v. 2015, p. 1, doi. 10.1155/2015/284863
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Flight Control Design for a Tailless Aircraft Using Eigenstructure Assignment.
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- International Journal of Aerospace Engineering, 2011, p. 1, doi. 10.1155/2011/549131
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Air Data Systems - Integrated Multi System Wireless Networks.
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- Electronics & Electrical Engineering, 2009, n. 95, p. 41
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An Automated Emergency Landing System for Fixed-Wing Aircraft: Planning and Control.
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- Journal of Field Robotics, 2015, v. 32, n. 8, p. 1114, doi. 10.1002/rob.21641
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Flight path control of small unmanned air vehicle.
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- Journal of Field Robotics, 2006, v. 23, n. 3/4, p. 223, doi. 10.1002/rob.20117
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Observations of surface momentum exchange over the marginal ice zone and recommendations for its parametrisation.
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- Atmospheric Chemistry & Physics, 2016, v. 16, n. 3, p. 1545, doi. 10.5194/acp-16-1545-2016
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Integrated interceptor guidance and control with prescribed performance.
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- International Journal of Robust & Nonlinear Control, 2015, v. 25, n. 16, p. 3179, doi. 10.1002/rnc.3260
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DYNAMIC CHARACTERISTICS OF OPERATOR'S "VISUAL CHANNEL" WHILE WORKING WITH TFT MONITOR.
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- Proceedings of National Aviation University, 2014, v. 1, n. 58, p. 44
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EXPERIMENTAL UNMANNED AERIAL VEHICLE FLIGHT DATA MEASUREMENT AND THEIR POST-PROCESSING ANALYSIS.
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- Proceedings of National Aviation University, 2014, v. 1, n. 58, p. 11
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SYNTHESIS OF KINEMATIC CONTROL OF AN AIRCRAFT IN "BIG".
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- Proceedings of National Aviation University, 2014, v. 1, n. 58, p. 17
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COMPUTER SIMULATION OF MODERN AIRCRAFTS BY USING NETWORK TECHNOLOGIES OF REMOTE CONTROL.
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- Proceedings of National Aviation University, 2013, v. 4, n. 57, p. 18
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ОЦІНКА ЯКОСТІ ТЕХНІКИ ПІЛОТУВАННЯ ЕКІПАЖУ В АВІАКОМПАНІЇ
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- Science-Based Technologies, 2020, v. 46, n. 2, p. 245, doi. 10.18372/2310-5461.46.14812
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Principles of Creation of Software for Processing Flight Information at the Flight Test Stage of Aerospace Systems.
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- Boundary Field Problems & Computer Simulation, 2012, v. 51, p. 84
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THE USE OF PILOT TRANSMISSION FUNCTION FOR AIRPLANE CONTROL DURING THE PROCESS OF AIMING.
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- Review of the Air Force Academy, 2010, v. 17, n. 1, p. 43
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Automatic control of the microaerial vehicles' attitude and position.
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- International Journal of Micro Air Vehicles, 2017, v. 9, n. 1, p. 61, doi. 10.1177/1756829316673847
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Design of a proportional-integral controller to track pitch angle in a mini aerial vehicle.
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- International Journal of Micro Air Vehicles, 2017, v. 9, n. 1, p. 15, doi. 10.1177/1756829316685181
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Passively Stable Flapping Flight From Hover to Fast Forward Through Shift in Wing Position.
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- International Journal of Micro Air Vehicles, 2015, v. 7, n. 4, p. 13, doi. 10.1260/1756-8293.7.4.407
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An Ecological Approach to the Supervisory Control of UAV Swarms.
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- International Journal of Micro Air Vehicles, 2014, v. 6, n. 4, p. 211, doi. 10.1260/1756-8293.6.4.211
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Development and Testing of a Quad Rotor Smartphone Control System for Novice Users.
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- International Journal of Micro Air Vehicles, 2012, v. 4, n. 3, p. 165, doi. 10.1260/1756-8293.4.3.165
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Simulation Analysis for UAV Search Algorithm Design Using Approximate Dynamic Programming.
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- Military Operations Research, 2009, v. 14, n. 2, p. 41, doi. 10.5711/morj.14.2.41
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Robust Multivariable Controller Design with the simultaneous H<sub>2</sub>/H<sub>∞</sub>/µ for a Single Person Aircraft.
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- International Journal of Electrical & Computer Engineering (2088-8708), 2013, v. 3, n. 2, p. 279
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Influence of Damping Over the Rudder Control System of an Aircraft.
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- Romanian Journal of Acoustics & Vibration, 2015, v. 12, n. 1, p. 10
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Adaptive control for a class of uncertain linear parameter-varying flight aircraft systems.
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- International Journal of Adaptive Control & Signal Processing, 2017, v. 31, n. 2, p. 210, doi. 10.1002/acs.2693
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Multivariable adaptive output rejection of unmatched input disturbances.
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- International Journal of Adaptive Control & Signal Processing, 2016, v. 30, n. 8-10, p. 1203, doi. 10.1002/acs.2590
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Adaptive backstepping flight control for a mini-UAV.
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- International Journal of Adaptive Control & Signal Processing, 2013, v. 27, n. 8, p. 635, doi. 10.1002/acs.2330
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