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hellow guys.. i need help!
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in the control input (u1,u2, u3, u4) of quadrotor UAV model the amlitude is very high how to reduce it, simulation is done on fixed step solver with in step time is 0.01 so how to optimize the control input that are force, roll torque, pitch torue and yaw torque, the controller used for controlling is SMC, if any one know about it help p/se?
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