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LQ Optimal Control
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Good evening, folks.
I want to ask a question related the design of an LQ optimal control.
I'm designing a system of a planar drone with 6 states and 2 inputs and despite the fact thay I understand the logic behind the weighting cost matrices Q and R, I am still getting numerical errors on Matlab and an instable behavior.
Does anybody know a practical method to get acceptable Q and R matrices using matlab?
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