Within the paper, the Soar architecture and Soar Intelligent Agents are introduced in section II. (2016), "Control computers diagnostics for UAV flight control system", Aircraft Engineering and Aerospace Technology, Vol. The main purpose of this paper is to present a novel approach to Automatic Flight Plan Generation, based on the fusion of a cognitive architecture with traditional control techniques. Competitive and innovative economy, 1.3 Regional innovation system. AbstractThe present paper describes the structure and the design aspects of a robust PID controller for higher-order systems. Numerical experiments were conducted with the use of MATLAB application, purchased during the realization of project number UDA-RPPK.01.03.00-18-003/10-00 “Construction, expansion and modernization of the scientific research base at Rzeszów University of Technology” is co-financed by the European Union from the European Regional Development Fund within Regional Operational Programme for the Podkarpacie Region for the years 2007-2013, I. Unmanned Aerial Vehicle (UAV) or often called an unmanned aircraft is a vehicle that can fly by being controlled using radio waves or flying autonomously. This scientific work has been financed from the Polish scientific funds for years 2010-2012 as a development project number OR00011611 Such technology demonstrator and flying laboratory enable different type of research in the area of aviation. The failure analysis of the flight control system of Air Force Institute of Technology (AFIT) UAV based on Markov analysis is elaborated in (Okafor & Eze, 2016). This paper presents the models and methods for reliability synthesis for components of UAV. Simulation results show that the modified NLDI flight control system is robust against wind disturbances and model mismatch and more accurately follows the desired path than CC and also requires the least control effort. The agent autonomously controls the UAV in an indoor envi-ronment and performs complex search and survey mis-sions. The designed system is the part of an UAV control system, designed for ground observation. The models and methods for reliability synthesis for components of UAV flight control system: flight computer and navigation system depict different variants of faulttolerant designs including designs for systems with complex reliability behavior. system and using the robot operating system (ROS).
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