The design of longitudinal autonomous landing control for a fixed wing Unmanned Aerial vehicle
Kangwei Chen
20212021 4th World Conference on Mechanical Engineering and Intelligent Manufacturing (WCMEIM)5 citationsDOI
Abstract
UAVs are frequently used in civil and military applications because of their tiny size, lightweight, and high mobility. In the field of aerospace, uncrewed aerial vehicles (UAVs) have become a central development direction. The takeoff and landing technology is a challenging issue in UAV control technology throughout the entire flight phase. The design and simulation of a UAV’s longitudinal landing control system are finished in this study by using PID theory and MATLAB Simulink, respectively.
Topics & Concepts
Fixed wingTakeoff and landingAerospaceTakeoffAeronauticsAerospace engineeringMATLABFlight control surfacesWingPID controllerLanding gearComputer scienceRemotely operated underwater vehicleControl systemEngineeringSimulationAutomotive engineeringAerodynamicsControl engineeringMobile robotRobotArtificial intelligenceElectrical engineeringTemperature controlOperating systemAdvanced Control Systems DesignAdaptive Control of Nonlinear SystemsReal-time simulation and control systems