A fighter plane is flying horizontally at a height of 250 m from ground with a constant velocity of 500 m/s. It passes exactly over a low-powered missile launcher which can fire a missile at any time in any direction with a speed of 100 m/s. Find the duration of time for which the plane is in danger of being hit by the missile in seconds.
Assumptions and Details
Gravitational field strength at Earth's surface is 10 m / s 2
The missile is not self-propelled
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I have a small doubt. The horizontal velocity of of the missile is always less than that of the plane so if the plane is flying directly above the launcher how can the missile ever reach it?
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I'll try to clear this doubt here
At any point of time, it is the relative velocity(particularly the velocity of approch), that determines whether the distance between the missile and the plane is increasing or decreasing.
So the small magnitude of missile's speed is immaterial
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Didn't get you. If the missile can never approach the plane, how will it hit?
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@Sai Prasanth Rao – It will definitely approach
I fixed some of the LaTeX. Great problem!
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Thanks. Couldn't figure out why the line wasn't working.
That equation describes the trajectory of a cannon shell (drag ignored), not that of a missile, which is self propelled and has variable mass, and a range. The wording is unfortunately misleading, I shall say......
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I fixed it. Better?
A small typo in the 2nd line. It will be d ( tan θ ) d y not d ( tan θ ) d x
Cud you please find out the fault in my reasoning? We need to find out the maximum horizontal distance x which can be covered by the missile, when it's vertical distance is fixed i.e y=250 m. Now, x = v cos θ t . Logically, x will be maximum when both v cos θ as well as t i.e. time taken is maximum. This means that v sin θ or vertical component of speed will have to be minimum. The min value of v sin θ needed to reach the given height= 2 g h = 2 × 1 0 × 2 5 0 = 5 0 2
Therefore, v cos θ = 1 0 0 2 − ( 5 0 2 ) 2 = 5 0 2
Time taken or t = v sin θ / g = 5 0 2 / 1 0 = 5 2 seconds. Thus, x = v cos θ t = 5 0 2 × 5 2 = 500 m, on one side.
therefore, total horizontal distance in which plane is in danger = 1000 m. So, plane should be in danger for a period of 1 0 0 0 / 5 0 0 = 2 seconds.
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If you look closely at your solution, you'll realize that you have solved the case when air plane is at the peak of the canon's trajectory... (I did the same mistake at my first attempt). But then, that's not the extreme case as the Canon can strike the plane while descending( which will surely yield a greater value of x)
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Yes, I had realised the same two days back, when I was discussing this with you. Thanks, anyways. :D
@Mayank Singh I did the same thing as sanchit but i can not understand the fault in my logic. Please elaborate and explain the fault.
Yea well same mistake as mine. Should have thought that the missile can hit the plane when it's falling back down. Btw, didnt you figure out the distance 1000m in a rather complex way.??Easy to calculate if we think of it as twice the half of the range of 1 projectile, in the scenario where we fire 2 of them
Made the same mistake of assuming that the highest range is possible with θ = 4 5 degrees but in reality it occurs at ≈ 5 4 . 7 3 degrees.
We now that the equation of the trajectory of the missile is given by
y = x tan θ − 2 v 0 2 cos 2 θ g x 2
Given that the plane is in danger if the missile reaches y = 2 5 0 m, we can find a function x ( θ ) such that the missile reaches such height. If we derivate x ( θ ) with respect to θ and equalise to cero, we can find θ such that x is maximum. This value times 2 would be the range in which the fighter plane will be in danger.
So, substituting y = 2 5 0 , v 0 = 1 0 0 m/s and g = 1 0 m/s 2 , we get
2 5 0 = x tan θ − 2 ( 1 0 4 ) cos 2 θ 1 0 x 2
or better
x 2 − 1 0 0 0 sin 2 θ + 5 ( 1 0 5 ) cos 2 θ = 0 .
Solving for x we get
x ( θ ) = 5 0 0 ( sin 2 θ ± sin 2 2 θ − cos 2 θ ) .
Since we want the maximum value of x , we choose the + sign, and derivate equalising to cero to obtain θ = 2 tan − 1 ( 2 − 3 ) = 5 4 . 7 4 degrees, which gives x m a x to be 5 0 0 2 m.
Hence, as said, 1 0 0 0 2 m would be the range in which the fighter plane will be in danger, and therefore 2 2 = 2 . 8 2 8 seconds would be the duration of time for which the plane is in danger of being hit by the missile.
The missile will never reach the target.
why into 2 ?
Could you please explain without using the equation? Its a little difficult to understand.
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We first find the area in which the missile can reach. The equation of trajectory for the missile is
y = x tan θ − u 2 2 1 g x 2 sec 2 θ
For maximum y for a given x -
d ( tan θ ) d y = x − u 2 2 1 g x 2 ( 2 tan θ ) = 0
⇒ tan θ = g x u 2
Putting in the first equation, we have
y m a x = x g x u 2 − u 2 2 1 g x 2 [ 1 + g 2 x 2 u 4 ] = 2 g u 2 − u 2 2 1 g x 2
Therefore, the missile can hit an area given by
y ≤ 2 g u 2 − u 2 2 1 g x 2
Given the problem y = 2 5 0 m , u = 1 0 0 m / s , g = 1 0 m / s 2 . Putting these values we get,
2 0 0 0 x 2 ≤ 2 5 0 ⇒ − 5 0 0 2 ≤ x ≤ 5 0 0 2
Therefore, the plane is in danger for a period of 5 0 0 1 0 0 0 2 = 2 2 seconds.