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# Turgut Ataseven

Last seen: Today Active since 2021

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Implementing the Trapezoidal Method
Hi. The aim is to utilize Trapezoidal Method for an integral with no variables, so we will get the x after integration. where ...

circa un mese ago | 0 answers | 0

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Out of memory error
Hi, please do not mind long lines because most of them are loops. Whenever I run the code, it runs for approximately fo...

4 mesi ago | 0 answers | 0

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Index in position 2 exceeds array bounds (must not exceed 1).
Hi. First of all sorry for asking the same question again and again but I am really close to the solution (probably). ...

4 mesi ago | 1 answer | 0

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Unable to perform assignment because the indices on the left side are not compatible with the size of the right side.
Hi. First of all sorry for asking the same question again and again but I am really close to the solution (probably). Ple...

4 mesi ago | 1 answer | 0

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Question

Unable to perform assignment because the indices on the left side are not compatible with the size of the right side.
Hi. First of all sorry for asking the same question again and again but I am really close to the solution (probably). ...

4 mesi ago | 1 answer | 0

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Unable to perform assignment because the size of the left side is 1-by-1 and the size of the right side is 1-by-79201.
Hi. First of all sorry for asking the same question again and again but I am really close to the solution (maybe not). I have 2 ...

5 mesi ago | 0 answers | 0

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Question

Utilizing the Euler Method
Hi. First of all sorry for asking a huge question.I need a guide to utilize the Euler Method. I am having troubles with the ...

5 mesi ago | 2 answers | 0

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Index exceeds the number of array elements (391).
Hi all. That is my function: function [Vtas_cl] = Velocities(H1,H2) Vcl_1 = 335; % Standard calibrated airspeed ...

5 mesi ago | 1 answer | 0

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Question

Index exceeds the number of array elements (1).
Hi. My code tries to solve 6 ODEs with 6 state variables [horizontal position (x1 and x2), altitude (x3), the true airspeed (x4...

5 mesi ago | 1 answer | 0

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Question

Too many input arguments.
Hi. My code tries to solve 6 ODEs with 6 state variables [horizontal position (x1 and x2), altitude (x3), the true airspeed ...

5 mesi ago | 1 answer | 0

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Question

Cannot plot the full interval
function [] = FuelJetPlot H_climb = 0:500:35000; % Altitude [ft] for k1 = 1:length(H_climb) % CLIMB PHASE % Thru...

6 mesi ago | 1 answer | 0

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Question

Not enough input arguments.
function yp = predprey(t,y,a,b,c,d) h=0.0625;tspan=[0 40];y0=[2 1]; a=1.2;b=0.6;c=0.8;d=0.3; yp = [a*y(1)-b*y(1)*y(2);-c*...

12 mesi ago | 1 answer | 0