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Use published T200 data to map T -> U where U is pwm required for the desired thrust.
Might want a QP optimizer here for T?
min T (G*T - F)^2 s.t. T_min <= T <= T_max @Hermanoid thoughts?
The text was updated successfully, but these errors were encountered:
Cascaded PID controller
Steps:
[6x8] [8x1]=[6x1]
G is full-rank:
Use published T200 data to map T -> U where U is pwm required for the desired thrust.
Might want a QP optimizer here for T?
min T (G*T - F)^2 s.t. T_min <= T <= T_max
@Hermanoid thoughts?
The text was updated successfully, but these errors were encountered: