A projectile is launched from ground level at an angle with respect to ground. A uniform ambient gravity pulls downward on the projectile.
In addition, thrusters continuously supply a force in the direction of the projectile's instantaneous velocity. The magnitude of the thrust force is equal to half of the projectile's weight.
What angle (in degrees) maximizes the horizontal distance between the launch point and the landing point?
Note: Neglect air resistance. Also assume that the projectile mass remains constant.
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We need to solve the simultaneous differential equations m x ¨ = 2 x ˙ 2 + y ˙ 2 m g x ˙ m y ¨ = 2 x ˙ 2 + y ˙ 2 m g y ˙ − m g with x ( 0 ) = y ( 0 ) = 0 and x ˙ ( 0 ) = V cos θ , y ˙ ( 0 ) = V sin θ for some V > 0 . By rescaling the time and distance variables we can simplify the equations to x ¨ = 2 x ˙ 2 + y ˙ 2 x ˙ y ¨ = 2 x ˙ 2 + y ˙ 2 y ˙ − 1 with x ( 0 ) = y ( 0 ) = 0 and x ˙ ( 0 ) = 5 cos θ , y ˙ ( 0 ) = 5 sin θ . We then need to find the value T θ > 0 for which y ( T θ ) = 0 , and seek to maximize R ( θ ) = x ( T θ ) . Here is a plot of R ( θ ) .
This is subject to numerical analysis. Solving these equations numerically using Mathematica, we obtain that R is maximized when θ = 1 . 0 6 2 3 3 9 , which corresponds to 6 0 . 8 7 ∘ .