Works matching DE "FLIGHT control systems"
Results: 725
Research on the Damage Characteristics of a UAV Flight Control System Irradiated by a Continuous Laser.
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- Aerospace (MDPI Publishing), 2025, v. 12, n. 2, p. 161, doi. 10.3390/aerospace12020161
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Numerical modeling of the effect of geometric asymmetry on the damping aerodynamic characteristics of supersonic sectional flight vehicles.
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- Fluid Dynamics, 2006, v. 41, n. 3, p. 460, doi. 10.1007/s10697-006-0062-7
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Effectiveness of the Compound Helicopter Configuration in Rotorcraft Performance Increase.
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- Transactions on Aerospace Research, 2020, v. 2020, n. 4, p. 81, doi. 10.2478/tar-2020-0023
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Mathematical modeling and vertical flight control of a tilt-wing UAV.
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- Turkish Journal of Electrical Engineering & Computer Sciences, 2012, v. 20, n. 1, p. 149, doi. 10.3906/elk-1007-624
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A stationary, variable DOF flight control system for an unmanned quadrocopter.
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- Turkish Journal of Electrical Engineering & Computer Sciences, 2011, v. 19, n. 6, p. 891, doi. 10.3906/elk-1007-579
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Design of an On‑Board Vision‑Based Obstacle Avoidance System for Flapping‑Wing Robots.
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- Transactions of Nanjing University of Aeronautics & Astronautics, 2024, v. 41, n. 1, p. 97, doi. 10.16356/j.1005‑1120.2024.01.008
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Anti⁃icing/De⁃icing Mechanism and Application Progress of Bio⁃inspired Surface for Aircraft.
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- Transactions of Nanjing University of Aeronautics & Astronautics, 2022, v. 39, n. 5, p. 541, doi. 10.16356/j.1005‑1120.2022.05.004
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Research and Design of Coordinated Control Strategy for Smart Electromechanical Actuator System.
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- Transactions of Nanjing University of Aeronautics & Astronautics, 2022, v. 39, n. 5, p. 507, doi. 10.16356/j.1005‑1120.2022.05.001
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An Optimization Method of Formation Flight for Minimizing Fuel Consumption.
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- Transactions of Nanjing University of Aeronautics & Astronautics, 2021, v. 38, n. 2, p. 306, doi. 10.16356/j.1005-1120.2021.02.011
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Progress of Chinese “Dove” and Future Studies on Flight Mechanism of Birds and Application System.
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- Transactions of Nanjing University of Aeronautics & Astronautics, 2020, v. 37, n. 5, p. 663, doi. 10.16356/j.1005⁃1120.2020.05.001
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Oscillatory Failure Detection for Flight Control System Using Voting and Comparing Monitors.
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- Transactions of Nanjing University of Aeronautics & Astronautics, 2019, v. 36, n. 5, p. 817, doi. 10.16356/j.1005-1120.2019.05.013
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Drone Hacking: Mirai in the Sky?
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- ISSA Journal, 2020, v. 18, n. 1, p. 41
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Drone Hacking: Mirai in the Sky?
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- ISSA Journal, 2019, v. 17, n. 7, p. 14
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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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Fault-Tolerant Control for Quadrotor Based on Fixed-Time ESO.
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- Mathematics (2227-7390), 2022, v. 10, n. 22, p. 4386, doi. 10.3390/math10224386
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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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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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The results of flight tests of an attitude control system for the Chibis-M microsatellite.
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- Cosmic Research, 2014, v. 52, n. 3, p. 205, doi. 10.1134/S0010952514020038
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The Rate of Single Event Upsets in Electronic Circuits onboard Spacecraft.
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- Cosmic Research, 2005, v. 43, n. 6, p. 423, doi. 10.1007/s10604-005-0066-9
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Approximate Calculation of Required and Available Lateral Range Achieved in a Spacecraft Descent to a Preset Point on the Earth's Surface.
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- Cosmic Research, 2005, v. 43, n. 6, p. 442, doi. 10.1007/s10604-005-0068-7
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A System of Stabilizing the Angular Motion of a Spacecraft Based on a Neuron-like System of Autonomous Adaptive Control.
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- Cosmic Research, 2004, v. 42, n. 3, p. 269, doi. 10.1023/B:COSM.0000033301.16194.fc
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Optimal Control of a Programmed Turn of a Spacecraft.
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- Cosmic Research, 2003, v. 41, n. 2, p. 178, doi. 10.1023/A:1023391232053
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Monitoring the functional state of human operators by the parameters of the fundamental tone and spectrum of speech.
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- Human Physiology, 2009, v. 35, n. 2, p. 252, doi. 10.1134/S0362119709020170
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METHOD OF IMPROVING THE ACCURACY OF NAVIGATION MEMS DATA PROCESSING OF UAV INERTIAL NAVIGATION SYSTEM.
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- Radio Electronics, Computer Science, Control, 2022, n. 3, p. 196, doi. 10.15588/1607-3274-2022-3-18
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METHOD OF THE INTELLIGENT SYSTEM CONSTRUCTION OF AUTOMATIC CONTROL OF UNMANNED AIRCRAFT APPARATUS.
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- Radio Electronics, Computer Science, Control, 2019, n. 1, p. 218, doi. 10.15588/1607-3274-2019-1-20
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A Method for Aileron Actuator Fault Diagnosis Based on PCA and PGC-SVM.
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- Shock & Vibration, 2016, p. 1, doi. 10.1155/2016/4807250
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Evolution, types, and distribution of flight control devices on wings and elytra in bark beetles.
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- Scientific Reports, 2024, v. 14, n. 1, p. 1, doi. 10.1038/s41598-024-57658-y
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Design of controller switching strategy for reusable launch vehicle with elevon jamming failure.
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- Electrical Engineering in Japan, 2008, v. 164, n. 2, p. 80, doi. 10.1002/eej.20356
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AIRCRAFT DEPARTURE CONTROL SYSTEMS - HIDDEN SAFETY RISKS.
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- International Journal for Traffic & Transport Engineering, 2017, v. 7, n. 3, p. 298, doi. 10.7708/ijtte.2017.7(3).02
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Energy Safety Management: A Training Model to Improve Flight Safety.
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- Journal of Aviation Technology & Engineering, 2024, v. 13, n. 1, p. 31, doi. 10.7771/2159-6670.1287
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Robustness and perfect tracking with simple adaptive control in nonlinear systems.
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- Mathematics in Engineering, Science & Aerospace (MESA), 2018, v. 9, n. 1, p. 21
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Attitude guidance and control of the navigation satellites at a passage of the singular orbital sites.
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- Mathematics in Engineering, Science & Aerospace (MESA), 2017, v. 8, n. 1, p. 43
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Parallelization of Finding the Current Coordinates of the Lidar Based on the Genetic Algorithm and OpenMP Technology.
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- Symmetry (20738994), 2021, v. 13, n. 4, p. 666, doi. 10.3390/sym13040666
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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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Recent development of unmanned aerial vehicle for plant protection in East Asia.
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- International Journal of Agricultural & Biological Engineering, 2017, v. 10, n. 3, p. 18, doi. 10.3965/j.ijabe.20171003.3248
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ARRT Development for the Upcoming Human Exploration Missions.
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- Space Weather: The International Journal of Research & Applications, 2020, v. 18, n. 12, p. 1, doi. 10.1029/2020SW002586
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TCN-Informer-Based Flight Trajectory Prediction for Aircraft in the Approach Phase.
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- Sustainability (2071-1050), 2023, v. 15, n. 23, p. 16344, doi. 10.3390/su152316344
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Efficient Quadcopter Flight Control Using Hybrid SSVEP + P300 Visual Brain Computer Interface.
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- International Journal of Human-Computer Interaction, 2022, v. 38, n. 1, p. 42, doi. 10.1080/10447318.2021.1921482
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OBSERVER and NEURAL NETWORK BASED FAULT TOLERANT CONTROL APPLICATION on AIRCRAFT LONGITUDINAL FLIGHT CONTROL.
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- Journal of Aeronautics & Space Technologies / Havacilik ve Uzay Teknolojileri Dergisi, 2017, v. 10, n. 2, p. 61
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A NEW ALTERNATIVE AIR DATA COMPUTATION METHOD BASED ON ARTIFICIAL NEURAL NETWORKS.
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- Journal of Aeronautics & Space Technologies / Havacilik ve Uzay Teknolojileri Dergisi, 2017, v. 10, n. 1, p. 21
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SENSOR FAULTS DIAGNOSIS IN AIRCRAFT LATERAL FLIGHT CONTROL USING MODEL BASED APPROACHES.
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- Journal of Aeronautics & Space Technologies / Havacilik ve Uzay Teknolojileri Dergisi, 2015, v. 8, n. 1, p. 39
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DİKEY İNİŞ-KALKIŞ YAPABİLEN DÖRT ROTORLU HAVA ARACININ(QUADROTOR) UÇUŞ KONTROLÜ.
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- Journal of Aeronautics & Space Technologies / Havacilik ve Uzay Teknolojileri Dergisi, 2010, v. 4, n. 3, p. 33
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KANAT YUNUSLAMASI VE DEĞİŞKEN KANATÇIK AÇILARI SIRASINDA OLUŞAN BÜYÜK GİRDAP OLUŞUMLARININ SİMÜLASYONU.
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- Journal of Aeronautics & Space Technologies / Havacilik ve Uzay Teknolojileri Dergisi, 2009, v. 4, n. 1, p. 61
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UÇUŞ KONTROL SİSTEMİNDE BİLİNMEYEN GİRİŞ GÖZLEYİCİLERİ KULLANARAK ALGILAYICI ARIZASI TESPİTİ VE AYRIMI.
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- Journal of Aeronautics & Space Technologies / Havacilik ve Uzay Teknolojileri Dergisi, 2007, v. 3, n. 2, p. 17
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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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Comparison of Classical PD and Fuzzy PD Controller Performances of an Aircraft Pitch Angle Control System.
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- Gazi University Journal of Science, 2011, v. 24, n. 4, p. 781
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- Article
Comparison of the Linear Homing, Parabolic Homing and Proportional Navigation Guidance Methods on a Two-Part Homing Missile against a Surface Target.
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- Gazi University Journal of Science, 2010, v. 23, n. 1, p. 81
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Seasprites in Antarctica.
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- Wings of Gold, 2018, v. 43, n. 3, p. 16
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REGULATIONS FOR OPERATION OF AIRCRAFT.
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- Wings of Gold, 2017, v. 42, n. 1, p. 17
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- Article