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For some quadrotor UAVs with relatively partial center of gravity, the impact of inertia product should be considered. I_xy,I_xz, I_yz can't just be considered 0(Maybe I misunderstood the code)
The text was updated successfully, but these errors were encountered:
For some quadrotor UAVs with relatively partial center of gravity, the impact of inertia product should be considered. I_xy,I_xz, I_yz can't just be considered 0(Maybe I misunderstood the code)
The text was updated successfully, but these errors were encountered: