Works matching DE "HELICOPTER control systems"
Results: 88
Simulation and system identification of helicopter dynamics using support vector regression.
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- Aeronautical Journal, 2015, v. 119, n. 1222, p. 1541, doi. 10.1017/S0001924000011398
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Validation of mathematical models for helicopter flight simulators past, present and future challenges.
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- Aeronautical Journal, 2013, v. 117, n. 1190, p. 343, doi. 10.1017/S0001924000008058
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Predictive inverse simulation of helicopters in aggressive manoeuvring flight.
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- Aeronautical Journal, 2012, v. 116, n. 1175, p. 87, doi. 10.1017/S0001924000006631
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Non-linear control algorithm for the four rotors UAV attitude tracking problem.
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- Aeronautical Journal, 2011, v. 115, n. 1165, p. 175, doi. 10.1017/S0001924000005571
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Investigation of rotorcraft-pilot couplings under flight-path constraint below the minimum-power speed.
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- Aeronautical Journal, 2010, v. 114, n. 1157, p. 405, doi. 10.1017/S0001924000003882
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Load transportation system based on autonomous small size helicopters.
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- Aeronautical Journal, 2010, v. 114, n. 1153, p. 191, doi. 10.1017/S0001924000003638
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Simulation of automatic helicopter deck landings using nature inspired flight control.
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- Aeronautical Journal, 2010, v. 114, n. 1151, p. 25
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Interactional aerodynamics and acoustics of a hingeless coaxial helicopter with an auxiliary propeller in forward flight.
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- Aeronautical Journal, 2009, v. 113, n. 1140, p. 65, doi. 10.1017/S0001924000002797
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Derivation of control activity metrics for the rule-based prediction of helicopter pilot workload.
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- Aeronautical Journal, 2004, v. 108, n. 1083, p. 245, doi. 10.1017/S0001924000005108
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Modeling and experimental investigation of a controllable rotary fluid damper.
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- Archives of Mechanics, 2023, v. 75, n. 4, p. 493, doi. 10.24423/aom.4216
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Modeling and Experimental Verification of a Semi-rotary Fluid Damper Based on an Improved Kelvin Model.
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- Arabian Journal for Science & Engineering (Springer Science & Business Media B.V. ), 2021, v. 46, n. 8, p. 7587, doi. 10.1007/s13369-021-05414-z
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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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A MODEL PREDICTIVE FRAMEWORK FOR AUTONOMOUS 3D FORMATION FLIGHT OF HELICOPTER GROUPS.
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- Control & Intelligent Systems, 2009, v. 37, n. 4, p. 220
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Singularity-free non-linear controller for a model-scaled autonomous helicopter.
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- IET Control Theory & Applications (Wiley-Blackwell), 2016, v. 10, n. 2, p. 210, doi. 10.1049/iet-cta.2015.0565
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Robust output-feedback attitude control of a three-degree-of-freedom helicopter via sliding-mode observation technique.
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- IET Control Theory & Applications (Wiley-Blackwell), 2015, v. 9, n. 11, p. 1637, doi. 10.1049/iet-cta.2014.1068
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Design of a Stability Augmentation System for an Unmanned Helicopter Based on Adaptive Control Techniques.
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- Applied Sciences (2076-3417), 2015, v. 5, n. 3, p. 575, doi. 10.3390/app5030575
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Hover Control for Helicopter Using Neural Network-Based Model Reference Adaptive Controller.
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- Iraqi Journal for Electrical & Electronic Engineering, 2017, v. 13, n. 1, p. 67, doi. 10.33762/eeej.2017.128789
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An unmanned helicopter control with partial small body force compensation: Experimental results.
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- Robotica, 2018, v. 36, n. 10, p. 1436, doi. 10.1017/S0263574718000486
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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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Closed-Loop Behavior of an Autonomous Helicopter Equipped with a Robotic Arm for Aerial Manipulation Tasks.
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- International Journal of Advanced Robotic Systems, 2013, v. 10, n. 2, p. 1, doi. 10.5772/53754
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Autonomous Navigation, Guidance and Control of Small Electric Helicopter.
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- International Journal of Advanced Robotic Systems, 2013, v. 10, n. 1, p. 1, doi. 10.5772/54713
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A New Hybrid Control Architecture to Attenuate Large Horizontal Wind Disturbance for a Small-Scale Unmanned Helicopter.
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- International Journal of Advanced Robotic Systems, 2012, v. 9, n. 7, p. 1, doi. 10.5772/51316
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Quad-Rotor Unmanned Aerial Vehicle Helicopter Modelling & Control.
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- International Journal of Advanced Robotic Systems, 2011, v. 8, n. 4, p. 139, doi. 10.5772/45710
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Mathematical modeling and machining parameter optimization for the surface roughness of face gear grinding.
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- International Journal of Advanced Manufacturing Technology, 2017, v. 90, n. 9-12, p. 2453, doi. 10.1007/s00170-016-9576-2
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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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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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Adaptive Neural Fault-Tolerant Control for the Yaw Control of UAV Helicopters with Input Saturation and Full-State Constraints.
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- Applied Sciences (2076-3417), 2020, v. 10, n. 4, p. 1404, doi. 10.3390/app10041404
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Disturbance observer-based boundary control for a suspension cable system moving in the horizontal plane.
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- Transactions of the Institute of Measurement & Control, 2019, v. 41, n. 2, p. 340, doi. 10.1177/0142331218759823
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Adaptive Sliding Mode Observer-Based Robust Fault Reconstruction for a Helicopter With Actuator Fault.
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- Asian Journal of Control, 2016, v. 18, n. 4, p. 1558, doi. 10.1002/asjc.1243
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Monocular Camera based Trajectory Tracking of 3- DOF Helicopter.
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- Asian Journal of Control, 2014, v. 16, n. 3, p. 742, doi. 10.1002/asjc.857
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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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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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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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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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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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Simple Learning-Based Robust Trajectory Tracking Control of a 2-DOF Helicopter System.
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- Electronics (2079-9292), 2022, v. 11, n. 13, p. N.PAG, doi. 10.3390/electronics11132075
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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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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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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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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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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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Robust backstepping decentralized tracking control for a 3-DOF helicopter.
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- Nonlinear Dynamics, 2015, v. 82, n. 1/2, p. 947, doi. 10.1007/s11071-015-2209-8
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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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Optimal Control System Design Using A Genetic Algorithm.
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- ZAMM -- Journal of Applied Mathematics & Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1998, v. 78, p. 1035, doi. 10.1002/zamm.19980781586
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