Problem 2: Rate of momentum change for optimal control problem
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Envisage the below figure as free body diagram of an aircraft:
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likewise consider the shown axes and vectors, for at :
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Show that .
According to the above figure, we can survey these two cases at and , the velocity of the aircraft after will reach to and the angle between the aircraft and horizontal axis will reach to the . Thus, regarding generated angle between two velocity vectors, we can write:
The amount of can be neglected in front of .
On the other hand, momentum is defined as . So, we have:
Assuming the amount of to be negligible in front of changes in velocity;
Finally, we can summarize the answer as:
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Solved and typed by - Egm6341.s10.Team4.nimaa&m 03:08, 3 April 2010 (UTC)
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Problem 7: Expression for Hermitian interpolation at
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Consider the Hermitian interpolation by the following equation (on slide 35-2):
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Show the following expression can be obtained for :
By differentiating from the equation for , we will attain:
Now, we can compute the followings:
The acquired foregoing equation is equal to RHS of the expression. Now, we can compute the LHS of it as:
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Solved and typed by - Egm6341.s10.Team4.nimaa&m 04:15, 3 April 2010 (UTC)
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Problem 8: Expression for derivative of Hermitian interpolation at
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Consider the Hermitian interpolation by the following equation (on slide 35-2):
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Show the following expression can be obtained for :
By differentiating from the equation for , we will attain:
Now, we can compute the followings:
The acquired foregoing equation is equal to RHS of the expression. Now, we can compute the LHS of it as:
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Solved and typed by - Egm6341.s10.Team4.nimaa&m 04:23, 3 April 2010 (UTC)
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