UAVs can vary in size from those which can be hand launched to purpose built or adapted vehicles the size of conventional fixed or rotary wing aircraft. In recent years, the tendency to refer to any UAV as a "drone" has developed but the term is not universally considered appropriate. UAS can also include an autonomous UAV or, more likely, a semi autonomous UAV. These systems include, but are not limited to, remotely piloted air systems (RPAS) in which the UAV is controlled by a 'pilot' using a radio data link from a remote location. A command and control (C2) system - sometimes referred to as a communication, command and control (C3) system - to link the two.An autonomous or human-operated control system which is usually on the ground or a ship but may be on another airborne platform.Source: Regulation (EU) 2019/945 DescriptionĪn Unmanned Aerial System (UAS) has three components: Unmanned aircraft (UA) means any aircraft operating or designed to operate autonomously or to be piloted remotely without a pilot on board. 161–198.Unmanned aircraft system (UAS) means an unmanned aircraft and the equipment to control it remotely. "Background information and user guide for MIL-F-8785C", Military Specification – Flying Qualities of Piloted Airplanes. Heidelberg – New York: Physica-Verl., 2002. Neuro-fuzzy architectures and hybrid learning. Proceedings of the National Aviation University, 4, pp. "Design of UAV robust autopilot based on adaptive neuro-fuzzy inference system". of Research in Engineering and Technology, 5 (9), pp. "Autonomous intelligent flight control of fixed-wing UAV based on adaptive neuro-fuzzy inference system". IEEE Transactions on Systems, Man, and Cybernetics, 23, pp. "ANFIS: Adaptive network-based fuzzy inference system". Essentials of Fuzzy Modeling and Control. "Robust stabilization and optimization of flight control system with state feedback and fuzzy logics". Electronics and Control Systems, 3(41), pp. "On structures of combined UAV flight control systems with elements of fuzzy logics". Berlin: Heidelberg, New York: Springer-Verlag, pp. "Hard and soft computing in the robust flight control systems". "Linear quadratic suboptimal control with static output feedback". Electronics and Control Systems, 1(43), pp. "Observer-based flight control system design under LMI approach". Electronics and Control Systems, 3(37), pp. "Flight control system design via LMI-approach". Electronics and Control Systems, 2(44), pp. "Optimal guaranteed cost control of aircraft motion". Transactions of the Institute of Measurement and Control, 29 (1), pp. "Design of a robust static output feedback controller in the case of multiple parametric uncertainties". "Static output feedback stabilization with H performance for a class of plants". "Robust control and H optimization –Tutorial Paper". Automation and Information Sciences, 36(3), pp. "Multi-model approach to parametric robust optimization of digital flight control systems". KSAS (Korean Society on Aerospace Science), 2 (2), pp. "Parametric optimization procedure for robust flight control system design". Princeton University Press, Princeton, 300 p.ģ. John Wiley & Sons Ltd, Chichester, UK, 332 p.Ģ. Unmanned Aircraft Systems: UAVS Design, Development and Deployment.
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