User:Egm6341.s10.Team4.nimaa&m/HW6
Contents |
Problem 2: Rate of momentum change for optimal control problem[edit]
Given[edit]
Envisage the below figure as free body diagram of an aircraft:
likewise consider the shown axes and vectors, for
at
:
Find[edit]
Show that
.
Solution[edit]
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:
-
.
Author[edit]
Solved and typed by - Egm6341.s10.Team4.nimaa&m 03:08, 3 April 2010 (UTC) .
Problem 7: Expression for Hermitian interpolation at
[edit]
Given[edit]
Consider the Hermitian interpolation by the following equation (on slide 35-2):
Find[edit]
Show the following expression can be obtained for
:
Solution[edit]
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:
-
.
Author[edit]
Solved and typed by - Egm6341.s10.Team4.nimaa&m 04:15, 3 April 2010 (UTC) .
Problem 8: Expression for derivative of Hermitian interpolation at
[edit]
Given[edit]
Consider the Hermitian interpolation by the following equation (on slide 35-2):
Find[edit]
Show the following expression can be obtained for
:
Solution[edit]
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:
-
.
Author[edit]
Solved and typed by - Egm6341.s10.Team4.nimaa&m 04:23, 3 April 2010 (UTC) .






























