This is war!

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 m/s^2

  • The missile is not self-propelled


The answer is 2.828.

This section requires Javascript.
You are seeing this because something didn't load right. We suggest you, (a) try refreshing the page, (b) enabling javascript if it is disabled on your browser and, finally, (c) loading the non-javascript version of this page . We're sorry about the hassle.

2 solutions

Sharky Kesa
Feb 23, 2015

We first find the area in which the missile can reach. The equation of trajectory for the missile is

y = x tan θ 1 2 g x 2 u 2 sec 2 θ y = x \tan \theta - \dfrac {\frac {1}{2} g x^2}{u^2} \sec^2 \theta

For maximum y y for a given x x -

d y d ( tan θ ) = x 1 2 g x 2 u 2 ( 2 tan θ ) = 0 \dfrac {\mathrm{d} y}{\mathrm{d} (\tan \theta)} = x - \dfrac {\frac {1}{2} g x^2}{u^2} (2 \tan \theta) = 0

tan θ = u 2 g x \Rightarrow \tan \theta = \dfrac {u^2}{gx}

Putting in the first equation, we have

y m a x = x u 2 g x 1 2 g x 2 u 2 [ 1 + u 4 g 2 x 2 ] = u 2 2 g 1 2 g x 2 u 2 y_{max} = x \dfrac {u^2}{gx} - \dfrac {\frac {1}{2} g x^2}{u^2} \left[1 + \dfrac {u^4}{g^2 x^2} \right] = \dfrac {u^2}{2g} - \dfrac {\frac {1}{2} g x^2}{u^2}

Therefore, the missile can hit an area given by

y u 2 2 g 1 2 g x 2 u 2 y \leq \dfrac {u^2}{2g} - \dfrac {\frac {1}{2} g x^2}{u^2}

Given the problem y = 250 m , u = 100 m / s , g = 10 m / s 2 y = 250m, u = 100m/s, g = 10m/s^2 . Putting these values we get,

x 2 2000 250 500 2 x 500 2 \dfrac {x^2}{2000} \leq 250 \Rightarrow -500 \sqrt{2} \leq x \leq 500 \sqrt{2}

Therefore, the plane is in danger for a period of 1000 2 500 = 2 2 \dfrac {1000 \sqrt{2}}{500} = 2 \sqrt{2} seconds.

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?

Sai Prasanth Rao - 5 years, 4 months ago

Log in to reply

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

Mayank Singh - 5 years, 4 months ago

Log in to reply

Didn't get you. If the missile can never approach the plane, how will it hit?

Sai Prasanth Rao - 5 years, 3 months ago

Log in to reply

@Sai Prasanth Rao It will definitely approach

Mayank Singh - 5 years, 3 months ago

I fixed some of the LaTeX. Great problem!

Jake Lai - 6 years, 3 months ago

Log in to reply

Thanks. Couldn't figure out why the line wasn't working.

Sharky Kesa - 6 years, 3 months ago

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......

Luciano Riosa - 6 years, 3 months ago

Log in to reply

I fixed it. Better?

Sharky Kesa - 6 years, 3 months ago

Log in to reply

Nice, That's fairly OK now : )

Luciano Riosa - 6 years, 3 months ago

A small typo in the 2nd line. It will be d y d ( tan θ ) \dfrac {\mathrm{d} y}{\mathrm{d} (\tan \theta)} not d x d ( tan θ ) \dfrac {\mathrm{d} x}{\mathrm{d} (\tan \theta)}

Pranav Saxena - 4 years, 3 months ago

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 x=v \cos \theta t . Logically, x will be maximum when both v cos θ v \cos \theta as well as t i.e. time taken is maximum. This means that v sin θ v \sin \theta or vertical component of speed will have to be minimum. The min value of v sin θ v \sin \theta needed to reach the given height= 2 g h \sqrt {2gh} = 2 × 10 × 250 \sqrt {2 \times 10 \times 250} = 50 2 50\sqrt {2}

Therefore, v cos θ = 10 0 2 ( 50 2 ) 2 v \cos \theta = \sqrt {100^{2} - (50\sqrt {2})^{2}} = 50 2 50\sqrt {2}

Time taken or t = v sin θ / g t = v \sin \theta / g = 50 2 / 10 50 \sqrt {2} /10 = 5 2 5 \sqrt {2} seconds. Thus, x = v cos θ t x= v \cos \theta t = 50 2 × 5 2 50 \sqrt {2} \times 5 \sqrt {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 1000 / 500 1000/500 = 2 seconds.

Sanchit Aggarwal - 5 years, 11 months ago

Log in to reply

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)

Mayank Singh - 5 years, 11 months ago

Log in to reply

Yes, I had realised the same two days back, when I was discussing this with you. Thanks, anyways. :D

Sanchit Aggarwal - 5 years, 11 months ago

@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.

Anurag Bisht - 3 years, 8 months ago

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

Pranav Saxena - 4 years, 3 months ago

Made the same mistake of assuming that the highest range is possible with θ = 45 \theta=45 degrees but in reality it occurs at 54.73 \approx 54.73 degrees.

Harsh Poonia - 2 years, 3 months ago

We now that the equation of the trajectory of the missile is given by

y = x tan θ g x 2 2 v 0 2 cos 2 θ y=x \tan\theta-\dfrac{g x^2}{2 v_0^2\cos^2\theta}

Given that the plane is in danger if the missile reaches y = 250 y=250 m, we can find a function x ( θ ) x(\theta) such that the missile reaches such height. If we derivate x ( θ ) x(\theta) with respect to θ \theta and equalise to cero, we can find θ \theta such that x x is maximum. This value times 2 2 would be the range in which the fighter plane will be in danger.

So, substituting y = 250 y=250 , v 0 = 100 v_0=100 m/s and g = 10 g=10 m/s 2 ^2 , we get

250 = x tan θ 10 x 2 2 ( 1 0 4 ) cos 2 θ 250=x \tan\theta-\dfrac{10 x^2}{2 (10^4)\cos^2\theta}

or better

x 2 1000 sin 2 θ + 5 ( 1 0 5 ) cos 2 θ = 0 x^2-1000\sin2\theta+5(10^5)\cos^2\theta=0 .

Solving for x x we get

x ( θ ) = 500 ( sin 2 θ ± sin 2 2 θ cos 2 θ ) x(\theta)=500(\sin2\theta\pm\sqrt{\sin^22\theta-\cos^2\theta}) .

Since we want the maximum value of x x , we choose the + + sign, and derivate equalising to cero to obtain θ = 2 tan 1 ( 2 3 ) = 54.74 \theta =2 \tan ^{-1}\left(\sqrt{2-\sqrt{3}}\right)=54.74 degrees, which gives x m a x x_{max} to be 500 2 500\sqrt{2} m.

Hence, as said, 1000 2 1000\sqrt{2} m would be the range in which the fighter plane will be in danger, and therefore 2 2 = 2.828 2\sqrt{2}=2.828 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.

aniket chauhan - 5 years ago

Log in to reply

It will. Why do you think otherwise??

Pranav Saxena - 4 years, 3 months ago

why into 2 ?

Priyanka Chaudhary - 3 years, 11 months ago

Log in to reply

Both negative and positive values of x

Pranav Saxena - 3 years, 11 months ago

Could you please explain without using the equation? Its a little difficult to understand.

Anurag Bisht - 3 years, 8 months ago

0 pending reports

×

Problem Loading...

Note Loading...

Set Loading...