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2

This problem can be conveniently solved by resorting to a state-feedback controller as the one depicted below. In this case, we have that $P=\frac{1}{m \cdot s^2}$, $x=\left[ z, \dot{z} \right]^T$, $K=\left[k_p, k_d\right]$, $k_f=\frac{k_p}{m}$. Then, we need to apply the feed-forward term $v=mg$ to counteract the gravity. We end up with the transfer ...

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A disturbance yaw rate of $-0.1, \text{deg/s}$ seems way low. Are sure that in steady-state there won't be any cause external to your copter (very low airflow?) justifying it? Imbalance between the RPMs provided by the motors (max current not reached) ❌ The open-loop response of different motors will certainly vary because of the variability of the building ...

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You should probably check out the universities below. I have read about some great research work done in the field of Aerial Robotics in these universities. They might not have a separate program as such for Aerial Robotics but there's extensive amount of projects that several students and researchers take part in under this area, be it through the ...

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there seems to be no mature drone platform focused on the NN research personally I suggest using a drone combines a NUC, TX2 for example the drone works as a flying platform providing control APIs, and a gimble system if possible the vision system can be constructed by NUC, you can put your own camera on it and do your NN research for this design, you ...

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