Projectile on inclined plane — modified equations and trajectory analysis

hardJEE-MAINJEE-ADVANCED3 min read

Question

A projectile is launched from the base of an inclined plane (angle β\beta with horizontal) at an angle α\alpha with the incline. Derive the time of flight, range along the incline, and the condition for maximum range.

(JEE Advanced 2022 had a projectile-on-incline problem; JEE Main tests this 1-2 times per year)


Solution — Step by Step

Choose the right coordinate system

The trick: take axes along and perpendicular to the incline, not horizontal and vertical.

  • x-axis: along the incline (upward positive)
  • y-axis: perpendicular to the incline

In this frame, gg has two components:

  • Along incline: gsinβg\sin\beta (decelerating the projectile along x)
  • Perpendicular to incline: gcosβg\cos\beta (pulling it back to the surface)

Initial velocity components

If the launch speed is uu at angle α\alpha with the incline:

ux=ucosα,uy=usinαu_x = u\cos\alpha, \quad u_y = u\sin\alpha

The motion along the incline and perpendicular to it can now be treated independently.

Time of flight — when it returns to the incline

The projectile returns to the incline when y=0y = 0:

0=usinαT12gcosβT20 = u\sin\alpha \cdot T - \frac{1}{2}g\cos\beta \cdot T^2

T=2usinαgcosβT = \frac{2u\sin\alpha}{g\cos\beta}

Compare with flat ground: T=2usinα/gT = 2u\sin\alpha/g. The denominator now has gcosβg\cos\beta instead of gg.

Range along the incline

R=ucosαT12gsinβT2R = u\cos\alpha \cdot T - \frac{1}{2}g\sin\beta \cdot T^2

Substituting TT:

R=2u2sinαcos(α+β)gcos2βR = \frac{2u^2\sin\alpha\cos(\alpha+\beta)}{g\cos^2\beta}

Maximum range occurs when α=π4β2\alpha = \frac{\pi}{4} - \frac{\beta}{2}, i.e., the launch angle bisects the angle between the incline and the vertical.

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Why This Works

By aligning the coordinate system with the incline, we reduce the problem to standard projectile motion — just with a modified gravitational acceleration. Along the incline, gravity has component gsinβg\sin\beta (causing deceleration), and perpendicular to the incline, gcosβg\cos\beta acts like "effective gravity."

The condition for maximum range (α=45°β/2\alpha = 45° - \beta/2) can be understood geometrically: the optimal launch angle bisects the angle between the incline surface and the vertical. On flat ground (β=0\beta = 0), this gives α=45°\alpha = 45°, which is the familiar result.


Alternative Method

💡 Expert Tip

If you forget the incline formulas, you can always work in the standard horizontal-vertical frame. Set the incline equation as y=xtanβy = x\tan\beta, write x=ucos(α+β)tx = u\cos(\alpha+\beta)\cdot t and y=usin(α+β)t12gt2y = u\sin(\alpha+\beta)\cdot t - \frac{1}{2}gt^2, and find where the trajectory intersects the incline. This is longer but uses no new formulas.


Common Mistake

⚠️ Common Mistake

Students use the standard flat-ground formula R=u2sin2α/gR = u^2\sin 2\alpha / g for inclined plane problems. This does not apply. The range formula changes because (1) gravity has a component along the incline, and (2) the "ground" is now tilted. Also, the maximum range angle is NOT 45° — it is 45°β/245° - \beta/2. Using 45° on an incline gives a wrong answer.

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