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Study On Integrated Cumputer Aided Design For Unmanned Aircraft Control Systems

Posted on:2004-08-29Degree:MasterType:Thesis
Country:ChinaCandidate:M ZhangFull Text:PDF
GTID:2168360092976061Subject:Navigation, guidance and control
Abstract/Summary:PDF Full Text Request
This thesis studies the integrate flight control design platform applied in unmanned aircraft control systems. The platform is used to design hardware and software for unmanned aircraft control systems,and real-time simulation is also supplied,users can analyse the result of simulation and optimize the parameters of control law.The platform is made up of three parts:design platform,simulate platform and evaluate platform.the operate fation of design platform is pane with line ,it also supply the compile and check program;the simulate platform is to take real-time simulation based on the designed control system.
Keywords/Search Tags:Unmanned aircraft, Computer Aided Design, Simulation platform, the PID control, the flight control computer, Real-time simulation
PDF Full Text Request
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