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Dhruvilkumar Chavada


Last seen: 12日 前 |  2022 年からアクティブ

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altitude output problem with 6DOF EoM (Euler) fixed mass block.
I am using built in block from aerospace blockset for 6DOF euler angles with fixed mass for quadcopter. i have entered mass as...

4ヶ月 前 | 1 件の回答 | 0

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質問


PID altitude control of quadcopter
Hello everyone, I am designing a flight control algorithm for a UAV. In the first step, I am just designing control just altit...

4ヶ月 前 | 1 件の回答 | 0

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close the file with Callback in simulink
Hello, I am using command system('path &') to open a bin file before starting my simulation. (adding this under model propertie...

11ヶ月 前 | 1 件の回答 | 0

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質問


2D Finite Difference Method
%% Finite Difference Method syms x1 x2 x1_0 = 1; x2_0 = 1; tol = [0.0001;0.0001]; h = 0.1; a = zeros(2,10); a(1,1) = x1_0...

11ヶ月 前 | 1 件の回答 | 0

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