Works matching DE "FLIGHT control systems"
Results: 734
Fuzzy-PID side-stick force control for flight simulation.
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- Aeronautical Journal, 2016, v. 120, n. 1227, p. 845, doi. 10.1017/aer.2016.34
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Flight Dynamics, Simulation and Control: for Rigid and Flexible Aircraft.
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- 2015
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- Book Review
Pulse-frequency modulated guidance laws for a mortar missile with a pulse jet control mechanism.
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- Aeronautical Journal, 2015, v. 119, n. 1213, p. 389, doi. 10.1017/S0001924000010526
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Horizontal flight trajectories optimisation for commercial aircraft through a flight management system.
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- Aeronautical Journal, 2014, v. 118, n. 1210, p. 1499
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- Article
Multi-body dynamic modelling and flight control for an asymmetric variable sweep morphing UAV.
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- Aeronautical Journal, 2014, v. 118, n. 1204, p. 683, doi. 10.1017/S000192400000943X
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A hybrid approach for aircraft fault diagnosis based on fault inference and fault identification.
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- Aeronautical Journal, 2014, v. 118, n. 1199, p. 81, doi. 10.1017/S0001924000008940
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Stalling transport aircraft.
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- Aeronautical Journal, 2013, v. 117, n. 1198, p. 1183, doi. 10.1017/S0001924000008812
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Robust and computational efficient autopilot design: A hybrid approach based on classic control and genetic-fuzzy sliding mode control.
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- Aeronautical Journal, 2013, v. 117, n. 1194, p. 839, doi. 10.1017/S0001924000008484
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Towards understanding effects of non-linear flight control system elements on inexperienced pilots.
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- Aeronautical Journal, 2012, v. 116, n. 1185, p. 1201, doi. 10.1017/S0001924000007569
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Flight simulator study on the influence of vortex curvature on wake encounter hazard using LES wind fields.
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- Aeronautical Journal, 2012, v. 116, n. 1177, p. 287, doi. 10.1017/S0001924000006849
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Advanced Control of Aircraft, Spacecraft and Rockets.
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- 2012
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- Book Review
Multi sensor data fusion based approach for the calibration of airdata systems.
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- Aeronautical Journal, 2011, v. 115, n. 1164, p. 113, doi. 10.1017/S0001924000005509
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Wake vortex encounters in a flight simulator.
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- Aeronautical Journal, 2010, v. 114, n. 1159, p. 579, doi. 10.1017/S000192400000405X
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An innovative evaluation platform for new aircraft concepts.
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- Aeronautical Journal, 2010, v. 114, n. 1157, p. 451, doi. 10.1017/S0001924000003936
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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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- Article
A hybrid frequency-time domain technique for ground effect identification.
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- Aeronautical Journal, 2010, v. 114, n. 1156, p. 377, doi. 10.1017/S0001924000003833
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Flight control using pin-protuberances for blunted cones.
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- Aeronautical Journal, 2010, v. 114, n. 1154, p. 245, doi. 10.1017/S0001924000003699
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Performing co-ordinated turns with articulated wing-tips as multi-axis control effectors.
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- Aeronautical Journal, 2010, v. 114, n. 1151, p. 35, doi. 10.1017/S0001924000003511
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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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Towards Integrated design of fluidic flight controls for a flapless aircraft.
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- Aeronautical Journal, 2009, v. 113, n. 1149, p. 699, doi. 10.1017/S0001924000003365
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Control laws for a formation of autonomous flight vehicles.
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- Aeronautical Journal, 2009, v. 113, n. 1147, p. 609, doi. 10.1017/S0001924000003274
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Flight control system design with H∞ loop-shaping approach through non-diagonal weights.
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- Aeronautical Journal, 2009, v. 113, n. 1145, p. 447, doi. 10.1017/S0001924000003110
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Helicopter load alleviation using active control.
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- Aeronautical Journal, 2008, v. 112, n. 1137, p. 663, doi. 10.1017/S0001924000002633
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Generic stability and control for aerospace flight vehicle conceptual design.
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- Aeronautical Journal, 2008, v. 112, n. 1132, p. 293, doi. 10.1017/S000192400000227X
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Analysis of a reversible flight control system response to atmospheric turbulence.
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- Aeronautical Journal, 2008, v. 112, n. 1128, p. 93, doi. 10.1017/S0001924000002025
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Estimation of lateral-directional parameters using neural networks based modified delta method.
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- Aeronautical Journal, 2007, v. 111, n. 1124, p. 659, doi. 10.1017/S0001924000004838
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Survivability of helicopter with individual blade primary control failure.
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- Aeronautical Journal, 2007, v. 111, n. 1124, p. 645, doi. 10.1017/S0001924000004826
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Dynamic gain scheduled control of a Hawk scale model.
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- Aeronautical Journal, 2007, v. 111, n. 1121, p. 461, doi. 10.1017/S0001924000004723
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Rotorcraft simulation modelling and validation for control law design.
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- Aeronautical Journal, 2007, v. 111, n. 1116, p. 77, doi. 10.1017/S0001924000001780
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Aircraft flight characteristics in conditions of windshear and icing.
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- Aeronautical Journal, 2007, v. 111, n. 1115, p. 41, doi. 10.1017/S0001924000001743
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Longitudinal flight control design with handling quality requirements.
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- Aeronautical Journal, 2006, v. 110, n. 1111, p. 627
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A continuation design framework for nonlinear flight control problems.
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- Aeronautical Journal, 2006, v. 110, n. 1104, p. 85, doi. 10.1017/S0001924000001032
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Design criteria for conceptual sizing of primary flight controls.
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- Aeronautical Journal, 2004, v. 108, n. 1090, p. 629, doi. 10.1017/S0001924000000464
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Supersonic transport aircraft longitudinal flight control law design.
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- Aeronautical Journal, 2004, v. 108, n. 1084, p. 319, doi. 10.1017/S000192400000018X
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Fault Diagnosis and Reconfiguration in Flight Control Systems (Book).
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- 2004
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- Book Review
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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Load alleviation in tilt rotor aircraft through active control; modelling and control concepts.
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- Aeronautical Journal, 2004, v. 108, n. 1082, p. 169, doi. 10.1017/S0001924000000087
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Design of formation control laws for manoeuvred flight.
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- Aeronautical Journal, 2004, v. 108, n. 1081, p. 125
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- Article
Spacecraft control with constrained fast reorientation and accurate pointing.
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- Aeronautical Journal, 2004, v. 108, n. 1080, p. 85, doi. 10.1017/S0001924000005030
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Fault-Tolerant Flight Control Based on Two-Stage Approach and Interior Point Method.
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- Wireless Personal Communications, 2018, v. 102, n. 2, p. 1809, doi. 10.1007/s11277-017-5238-4
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- Article
طراحی کنترل کنندۀ غیرخطی سامانۀ کنترل پرواز موشک پدافندی با استفاده از روش فازی - تطبیقی براساس معادلات شش درجه آزادی
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- Computational Intelligence in Electrical Engineering, 2019, v. 10, n. 2, p. 19
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- Article
Improving Autonomous Performance of a Passive Morphing Fixed Wing UAV.
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- Information Technology & Control, 2020, v. 49, n. 1, p. 28, doi. 10.5755/j01.itc.49.1.23275
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- Article
Flight and Seizure Motor Patterns in Drosophila Mutants: Simultaneous Acoustic and Electrophysiological Recordings of Wing Beats and Flight Muscle Activity.
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- Journal of Neurogenetics, 2014, v. 28, n. 3/4, p. 316, doi. 10.3109/01677063.2014.957827
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- Article
Flight path optimization passing through waypoints for autonomous flight control systems.
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- Engineering Optimization, 2005, v. 37, n. 7, p. 755, doi. 10.1080/03052150500270479
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- Article
Optimum design of neural networks for a nonlinear flight control system.
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- Engineering Optimization, 2004, v. 36, n. 1, p. 1, doi. 10.1080/03052150310001627347
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- Article
Nonstationary flow field generated by dielectric barrier discharge.
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- Technical Physics Letters, 2011, v. 37, n. 5, p. 461, doi. 10.1134/S1063785011050282
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- Article
面向定量遥感的高分辨遥感综合定标场及其应用.
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- Journal of Remote Sensing, 2021, v. 25, n. 1, p. 198, doi. 10.11834/jrs.20210326
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- Article
Failure Detection of Composites with Control System Corrective Response in Drone System Applications †.
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- Computers (2073-431X), 2018, v. 7, n. 2, p. 23, doi. 10.3390/computers7020023
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- Article
A Way to Mitigate Force-Fight Oscillation Based on Pressure and Position Compensation for Fly-by-Wire Flight Control Systems.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2020, v. 63, n. 1, p. 1, doi. 10.2322/tjsass.63.1
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- Article
Efficiency Analysis of Speed Managed Descent in the Presence of Wind Prediction Error.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2018, v. 61, n. 1, p. 1, doi. 10.2322/tjsass.61.1
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- Article