Works matching DE "HELICOPTER control systems"
Results: 88
Adaptive Neural Control for an Uncertain 2-DOF Helicopter System with Unknown Control Direction and Actuator Faults.
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- Mathematics (2227-7390), 2022, v. 10, n. 22, p. 4342, doi. 10.3390/math10224342
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A Novel Comprehensive Kinematic and Inverse Dynamic Model for the Flybar-Less Swashplate Mechanism: Application on a Small-Scale Unmanned Helicopter.
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- Symmetry (20738994), 2020, v. 12, n. 11, p. 1849, doi. 10.3390/sym12111849
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SYNTHESIS OF OPTIMAL MULTIDIMENSIONAL STABILIZATION SYSTEM OF HELICOP-TER IN HOVERING MODE UNDER STOCHASTIC INFLUENCES.
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- Electronics & Control Systems, 2015, v. 44, n. 2, p. 51
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IMPROVING THE EFFICIENCY OF DEVELOPMENT PROCESS OF AUTOMATED HELICOPTER FLYING.
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- Electronics & Control Systems, 2014, v. 3, n. 41, p. 97, doi. 10.18372/1990-5548.41.7807
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Survey on Flight Control Technology for Large-Scale Helicopter.
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- International Journal of Aerospace Engineering, 2017, p. 1, doi. 10.1155/2017/5309403
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Study on Helicopter Antitorque Device Based on Cross-Flow Fan Technology.
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- International Journal of Aerospace Engineering, 2016, p. 1, doi. 10.1155/2016/5396876
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Dependable Low-altitude Obstacle Avoidance for Robotic Helicopters Operating in Rural Areas.
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- Journal of Field Robotics, 2013, v. 30, n. 3, p. 439, doi. 10.1002/rob.21455
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Channel Projection-Based CCA Target Identification Method for an SSVEP-Based BCI System of Quadrotor Helicopter Control.
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- Computational Intelligence & Neuroscience, 2019, p. 1, doi. 10.1155/2019/2361282
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Dynamic Comparative Analysis of Seven Equivalent Mechanisms of Swashplate.
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- International Journal of Simulation: Systems, Science & Technology, 2016, v. 17, n. 46, p. 1, doi. 10.5013/IJSSST.a.17.46.23
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Design Of Qft Controller For A Bench-Top Helicopter System Model.
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- International Journal of Simulation: Systems, Science & Technology, 2010, v. 11, n. 5, p. 8
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Nonlinear sliding sector design for multi‐input systems with application to helicopter control.
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- International Journal of Robust & Nonlinear Control, 2020, v. 30, n. 6, p. 2248, doi. 10.1002/rnc.4877
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Training a model-free reinforcement learning controller for a 3-degree-of-freedom helicopter under multiple constraints.
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- Measurement & Control (0020-2940), 2019, v. 52, n. 7/8, p. 844, doi. 10.1177/0020294019847711
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Design, development, and flight testing of a high endurance micro quadrotor helicopter.
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- International Journal of Micro Air Vehicles, 2016, v. 8, n. 3, p. 155, doi. 10.1177/1756829316653694
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STUDY OF DIFFERENT LOAD DEPENDENCIES AMONG SHARED REDUNDANT SYSTEMS.
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- Scalable Computing: Practice & Experience, 2009, v. 10, n. 3, p. 241
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Helicopter Laboratory Model Experiment with Web Access.
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- International Journal of Online Engineering, 2009, n. S1, p. 8, doi. 10.3991/ijoe.v5s1.1015
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Fuzzy Multi-model Switching H-Infinity Control for Helicopters in a Full Envelope.
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- Circuits, Systems & Signal Processing, 2013, v. 32, n. 5, p. 2185, doi. 10.1007/s00034-013-9558-7
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Elevation, pitch and travel axis stabilization of 3DOF helicopter with hybrid control system by GA-LQR based PID controller.
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- International Journal of Electrical & Computer Engineering (2088-8708), 2020, v. 10, n. 3, p. 1868, doi. 10.11591/ijece.v10i2.pp1868-1884
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Elevation, pitch and travel axis stabilization of 3DOF helicopter with hybrid control system by GA-LQR based PID controller.
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- International Journal of Electrical & Computer Engineering (2088-8708), 2020, v. 10, n. 2, p. 1868, doi. 10.11591/ijece.v10i2.pp1868-1884
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Dynamic Modeling and Flight Control Design for Multicopter.
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- International Review of Aerospace Engineering, 2018, v. 11, n. 5, p. 224, doi. 10.15866/irease.v11i5.15512
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Intelligent Control of Twin-Rotor MIMO System Using Fuzzy Inference Techniques.
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- International Review of Aerospace Engineering, 2013, v. 6, n. 1, p. 28
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HONEYWELL'S HEALTH AND USAGE MONITORING SYSTEMS SELECTED BY THE REPUBLIC OF SINGAPORE FOR ITS CH-47 FLEET.
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- Defence Review Asia, 2014, v. 8, n. 6, p. 6
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FRENCH HELICOPTERS IN COMBAT.
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- Defence Review Asia, 2011, v. 5, n. 8, p. 24
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ARMY AVIATION.
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- Defence Review Asia, 2011, v. 5, n. 6, p. 14
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Tribological behavior of aeronautical steel under oil-air lubrication containing extreme-pressure and anti-wear additives.
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- Advances in Mechanical Engineering (Sage Publications Inc.), 2016, v. 8, n. 8, p. 1, doi. 10.1177/1687814016638299
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Parallel blade-vortex interaction modelling for helicopter rotor noise control synthesis.
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- International Journal of Aeroacoustics, 2014, v. 13, n. 7/8, p. 587, doi. 10.1260/1475-472X.13.7-8.587
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Coaxial Helicopter Attitude Control System Design by Advanced Model Predictive Control under Disturbance.
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- Aerospace (MDPI Publishing), 2024, v. 11, n. 6, p. 486, doi. 10.3390/aerospace11060486
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Full State Constrained Flight Tracking Control for Helicopter Systems with Disturbances.
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- Aerospace (MDPI Publishing), 2023, v. 10, n. 5, p. 471, doi. 10.3390/aerospace10050471
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Preliminary Sizing of the Electrical Motor and Housing of Electromechanical Actuators Applied on the Primary Flight Control System of Unmanned Helicopters.
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- Aerospace (MDPI Publishing), 2022, v. 9, n. 9, p. 473, doi. 10.3390/aerospace9090473
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Formal Verification of Helicopter Automatic Landing Control Algorithm in Theorem Prover Coq.
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- International Journal of Performability Engineering, 2018, v. 14, n. 9, p. 1947, doi. 10.23940/ijpe.18.09.p2.19471957
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CONTROL DESIGN FOR UNMANNED AERIAL VEHICLES WITH FOUR ROTORS.
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- Interdisciplinary Description of Complex Systems, 2016, v. 14, n. 2, p. 236, doi. 10.7906/indecs.14.2.12
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Trajectory Tracking Control for Small-Scale Unmanned Helicopters with Mismatched Disturbances Based on a Continuous Sliding Mode Approach.
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- International Journal of Aerospace Engineering, 2019, p. 1, doi. 10.1155/2019/6235862
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Effect of the Simultaneous Variation in Blade Root Chord Length and Blade Taper on Helicopter Flight Control Effort.
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- International Journal of Aerospace Engineering, 2017, p. 1, doi. 10.1155/2017/6325269
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ACT/FHS System Identification Including Rotor and Engine Dynamics.
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- Journal of the American Helicopter Society, 2019, v. 64, n. 2, p. 1, doi. 10.4050/JAHS.64.022003
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Helicopter Fuselage Model Drag Reduction by Active Flow Control Systems.
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- Journal of the American Helicopter Society, 2019, v. 64, n. 2, p. 1, doi. 10.4050/JAHS.64.022001
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Formation Control of a Rotorcraft Multilift System.
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- Journal of the American Helicopter Society, 2017, v. 62, n. 4, p. 1, doi. 10.4050/JAHS.62.042011
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Prediction of Rotorcraft Design Impacts on Maneuverability Characteristics.
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- Journal of the American Helicopter Society, 2015, v. 60, n. 4, p. 1, doi. 10.4050/JAHS.60.042003
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Helicopter Slung Load Control Using Lagged Cable Angle Feedback.
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- Journal of the American Helicopter Society, 2015, v. 60, n. 2, p. 1, doi. 10.4050/JAHS.60.022011
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Eigenstructure Control: A Rotorcraft Handling Qualities Engineering Tool.
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- Journal of the American Helicopter Society, 2015, v. 60, n. 2, p. 1, doi. 10.4050/JAHS.60.022010
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A Real-Time Expert Control System For Helicopter Autorotation.
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- Journal of the American Helicopter Society, 2015, v. 60, n. 2, p. 1, doi. 10.4050/JAHS.60.022008
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Flight Control and Handling Qualities Evaluations Considering Air Resonance.
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- Journal of the American Helicopter Society, 2014, v. 59, n. 2, p. 022001-1, doi. 10.4050/JAHS.59.022001
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Mathematical Modeling of the NOTAR Antitorque System for Flight Simulation.
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- Journal of the American Helicopter Society, 2013, v. 58, p. 1, doi. 10.4050/JAHS.58.022002
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Rotorcraft Handling Qualities Engineering: Managing the Tension between Safety and Performance.
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- Journal of the American Helicopter Society, 2013, v. 58, n. 1, p. 1, doi. 10.4050/JAHS.58.011001
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- Article
the problem with power lines.
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- Electronics Letters (Wiley-Blackwell), 2015, p. 1041, doi. 10.1049/el.2015.2141
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- Article
Evaluation of polarisation characteristics of power-line RCS at 76 GHz for helicopter obstacle detection.
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- Electronics Letters (Wiley-Blackwell), 2015, p. 1110, doi. 10.1049/el.2015.1266
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Finite-Time Prescribed Performance Tracking Control for Unmanned Helicopter System Using Neural Network.
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- Processes, 2024, v. 12, n. 8, p. 1559, doi. 10.3390/pr12081559
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Fuzzy Control Design for a Class of Nonlinear Network Control System: Helicopter Case Study.
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- International Journal of Computers, Communications & Control, 2012, v. 7, n. 2, p. 365
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Synthesis of Adaptive Sliding Mode Control for Twin Rotor MIMO System with Mass Uncertainty based on Synergetic Control Theory.
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- International Journal of Robotics & Control Systems, 2024, v. 4, n. 1, p. 174, doi. 10.31763/ijrcs.v4i1.1307
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Helicopters Turboshaft Engines Neural Network Modeling under Sensor Failure.
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- Journal of Sensor & Actuator Networks, 2024, v. 13, n. 5, p. 66, doi. 10.3390/jsan13050066
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Use of Spatial Modelling to Select the Helicopter Landing Sites.
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- Advances in Military Technology, 2014, v. 9, n. 1, p. 69
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POTENTIAL FOR GREATNESS: THE NH90 FLEET IS SHOWING ITS PROMISE.
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- Asia-Pacific Defence Reporter, 2018, v. 44, n. 7, p. 34
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