Works matching DE "GUIDANCE systems (Flight)"
Results: 88
Performance comparison of the notable acceleration- and angle-based guidance laws for a short-range air-to-surface missile.
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- Turkish Journal of Electrical Engineering & Computer Sciences, 2017, v. 25, n. 5, p. 3591, doi. 10.3906/elk-1601-230
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A New Decoupling Matrix Construction Method for Fault Detection and Isolation of a Redundant Strapdown Inertial Measurement Unit.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2017, v. 60, n. 1, p. 60, doi. 10.2322/tjsass.60.60
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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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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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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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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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Air Force Purchases Upgrades for Raytheon-built Maverick Missiles.
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- Microwave Journal, 2004, v. 47, n. 3, p. 42
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- Article
Blind guidance system based on laser triangulation.
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- Optical Engineering, 2012, v. 51, n. 5, p. 1, doi. 10.1117/1.OE.51.5.054302
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THE ACTIVE FAULT TOLERANT CONTROL SYSTEM FOR PROCEEDING CONTROLLABILITY AND STABILITY AIRPLANE UNDER ADVERSE FLIGHT CONDITIONS.
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- Electronics & Control Systems, 2014, v. 1, n. 39, p. 33, doi. 10.18372/1990-5548.39.7327
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Smooth Adaptive Finite Time Guidance Law with Impact Angle Constraints.
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- International Journal of Aerospace Engineering, 2016, p. 1, doi. 10.1155/2016/5730168
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An Approximate Optimal Maximum Range Guidance Scheme for Subsonic Unpowered Gliding Vehicles.
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- International Journal of Aerospace Engineering, 2015, p. 1, doi. 10.1155/2015/389751
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Adaptive Integrated Guidance and Fault Tolerant Control Using Backstepping and Sliding Mode.
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- International Journal of Aerospace Engineering, 2015, p. 1, doi. 10.1155/2015/253478
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Development of Navigation and Automated Flight Control System Solutions for Maritime VTOL UAS Operations.
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- ITEA Journal of Test & Evaluation, 2013, v. 34, n. 1, p. 54
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Test and Evaluation of Fully Autonomous Micro Air Vehicles.
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- ITEA Journal of Test & Evaluation, 2008, v. 29, n. 4, p. 367
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A Biologically Inspired, Vision-based Guidance System for Automatic Landing of a Fixed-wing Aircraft.
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- Journal of Field Robotics, 2014, v. 31, n. 4, p. 699, doi. 10.1002/rob.21527
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Review of research on automatic guidance of agricultural vehicles.
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- Transactions of the Chinese Society of Agricultural Engineering, 2015, v. 31, n. 10, p. 1, doi. 10.11975/j.issn.1002-6819.2015.10.001
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EUROPEAN CENTRALIZED SERVICES OF AIR NAVIGATION SYSTEM.
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- Proceedings of National Aviation University, 2014, v. 60, n. 3, p. 43, doi. 10.18372/2306-1472.60.7563
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METHOD OF THE AIRCRAFT CONTROL RECONFIGURATION WHEN UNEXPECTED SITUATION APPEARS DURING FLIGHT.
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- Proceedings of National Aviation University, 2014, v. 2, n. 59, p. 44
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ANALYSIS OF THE ACCURACY'S CRITERIA OF THE FLIGHT CONTROL AND GUIDANCE SYSTEM.
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- Electronics & Control Systems, 2021, v. 70, n. 4, p. 71, doi. 10.18372/1990-5548.70.16774
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Control-oriented modelling and simulation of spacecraft attitude and orbit dynamics.
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- Mathematical & Computer Modelling of Dynamical Systems, 2006, v. 12, n. 1, p. 73, doi. 10.1080/13873950500071371
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Modifying the MARK 6 Guidance System.
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- EE: Evaluation Engineering, 2009, v. 48, n. 9, p. 22
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Influence of control strategy on stability of dual-spin projectiles with fixed canards.
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- Defence Technology, 2018, v. 14, n. 6, p. 709, doi. 10.1016/j.dt.2018.04.014
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Visual Apollo: A Graphical Exploration of Computer-Human Relationships.
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- Design Issues, 2014, v. 30, n. 2, p. 4, doi. 10.1162/DESI_a_00258
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Guidance Technology of Horizontal Curved Flight for Short Range Aircraft with Inertial Navigation.
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- Metallurgical & Mining Industry, 2015, n. 9, p. 112
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Improving performance on procedural tasks through presentation of locational procedure context: an empirical evaluation.
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- Behaviour & Information Technology, 2004, v. 23, n. 1, p. 11, doi. 10.1080/01449290310001641284
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Model-Based Actuator Fault Tolerant Robust Control Architecture: An Unmanned Aerial Vehicle Example.
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- International Review of Aerospace Engineering, 2009, v. 2, n. 4, p. 192
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An improved predictor-corrector entry guidance method for hypersonic flight vehicle.
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- Advances in Mechanical Engineering (Sage Publications Inc.), 2017, v. 9, n. 10, p. 1, doi. 10.1177/1687814017726291
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Atmospheric Reentry Dispersion Correction Ascent Phase Guidance for a Generic Reentry Vehicle.
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- Defence Science Journal, 2013, v. 63, n. 3, p. 233, doi. 10.14429/dsj.63.3733
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Intensive Asteroid Exploration.
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- International Review of Physics, 2012, v. 6, n. 5, p. 448
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DIAGNOSTICS OF FLY-BY-WIRE CONTROL SYSTEM.
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- Aviation (1648-7788), 2008, v. 12, n. 2, p. 41, doi. 10.3846/1648-7788.2008.12.41-45
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自动飞行模式转换逻辑的形式化建模与验证.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2023, v. 55, n. 5, p. 768, doi. 10.16356/j.1005‑2615.2023.05.003
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Online Deterministic 3D Trajectory Generation for Electric Vertical Take-Off and Landing Aircraft.
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- Aerospace (MDPI Publishing), 2024, v. 11, n. 2, p. 157, doi. 10.3390/aerospace11020157
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Development and Implementation of a Mission Data-Handling Algorithm for an Automatic Flight Guidance System.
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- Aerospace (MDPI Publishing), 2024, v. 11, n. 2, p. 115, doi. 10.3390/aerospace11020115
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RESEARCH ON SURFACE ROUGHNESS OF CIRCULAR ARC CUT BY ASJ.
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- Technical Gazette / Tehnički Vjesnik, 2016, v. 23, n. 3, p. 885, doi. 10.17559/TV-20141207083412
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A Stochastic Approach for Estimating the Effectiveness of a Route Guidance System and Its Related Parameters.
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- Transportation Science, 1985, v. 19, n. 4, p. 333, doi. 10.1287/trsc.19.4.333
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A Quango Unleashed: The Abolition of Policy Guidance in Civil Aviation Licensing.
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- Public Administration, 1980, v. 58, n. 3, p. 287, doi. 10.1111/j.1467-9299.1980.tb00407.x
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Mapping a Multilayer Air Transport Network with the Integration of Airway, Route, and Flight Network.
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- Journal of Applied Mathematics, 2019, p. 1, doi. 10.1155/2019/8282954
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Valuation of Real Options as Competitive Prototyping in System Development.
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- Defense Acquisition Research Journal: A Publication of the Defense Acquisition University, 2014, v. 21, n. 3, p. 668
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- Article
A Novel Control Scheme of Magnetic Lift and Guidance.
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- Electrical Engineering in Japan, 1992, v. 112, n. 3, p. 117, doi. 10.1002/eej.4391120313
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A Practical Adaptive Proportional-Derivative Guidance Law.
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- Engineering Letters, 2016, v. 24, n. 3, p. 102
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PROLBLEMS OF STABILIZATION OF SPACE VEHICLES WITH FLEXIBLE DYNAMICS. PART II. ROBUST AND NEURAL ADAPTIVE CONTROL.
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- Naukovi visti NTUU - KPI, 2006, v. 2006, n. 6, p. 61
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Sagem signs support contract for STRIX sights on Australian Tiger helicopters.
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- Asia-Pacific Defence Reporter, 2009, v. 35, n. 6, p. 8
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- Article
Unified approach to cooperative guidance laws against stationary and maneuvering targets.
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- Nonlinear Dynamics, 2015, v. 81, n. 4, p. 1635, doi. 10.1007/s11071-015-2096-z
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Guidance law with circular no-fly zone constraint.
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- Nonlinear Dynamics, 2014, v. 78, n. 3, p. 1953, doi. 10.1007/s11071-014-1571-2
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Optimization of the proportional navigation law with time delay.
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- Journal of Mathematical Sciences, 2007, v. 147, n. 2, p. 6644, doi. 10.1007/s10958-007-0501-y
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Energy-based approach for flight control systems design.
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- Automation & Remote Control, 2013, v. 74, n. 3, p. 372, doi. 10.1134/S0005117913030041
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The problem of motion correction with Gaussian communications channel.
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- Automation & Remote Control, 2011, v. 72, n. 2, p. 240, doi. 10.1134/S0005117911020044
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Modeling and analysis of the stress-strain state of robotic systems.
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- Przegląd Elektrotechniczny, 2021, v. 97, n. 8, p. 66, doi. 10.15199/48.2021.08.12
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Near Optimal Explicit Guidance Law with Impact Angle Constraints for a Hypersonic Re-entry Vehicle.
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- INCAS Bulletin, 2018, v. 10, n. 2, p. 39, doi. 10.13111/2066-8201.2018.10.2.5
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- Article