Robust Control of Vectored Thrust Aerial Vehicles via Sliding Mode Control
The aim of the research is to explore the applicability of Sliding Mode based methodologies to unmanned aerial vehicles. A vectored thrust aerial vehicle developed at UNSW in 2010 is used as the test platform for the research.
The final aim is to develop a nonlinear robust control methodology based on Sliding Modes which has improved convergence properties and eliminate current disadvantages of SMC.
Resulting Publications and Media (0)
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