Modeling and Control of VTOL Flying Wing with Thrust Vectoring
Master thesis
Permanent lenke
http://hdl.handle.net/11250/2616137Utgivelsesdato
2015Metadata
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Sammendrag
A simulator for the complete vehicle dynamics, as well as a flight control system, have been implemented in MATLAB/Simulink. The simulator enables easier development and testing of the control system, and provides valuable estimates of the total system performance. A physical prototype for concept validation is under development.