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My ultimate goal is to find the angle of elevation necessary to launch a projectile from the origin to (x,y) with initial velocity V and under gravitational acceleration g. Wind resistance is ignored.

This is where I've started, and the path I've taken. First, I took the parametrics for x and y.

x = V * cosθ * t

y = V * sinθ * t - (g / 2) * t^2

-Then, I found t in terms of x, V and θ...

t = x / (V * cosθ)

-I plugged that value in for t in the y equation...

y = V * sinθ* (x / (V * cosθ)) - (g / 2) * (x^2 / (V^2 * (cosθ)))

y = x * tan⁡θ - (g * x^2) / (2 * V^2 * (cos⁡θ)^2)

I don't know what to do from here. I need to find θ in terms of x, y, V, and g, but it seems impossible to get all of the θ's into a single term. (x, y, V and g will be known when I use the equation).

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    thanks, fixed that error, the one that's up now is what I have. The question issue is fixed (see end of post)2011-11-17

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Our equation looks like $y=x\tan\theta+\dfrac{k}{\cos^2\theta}x^2$ for a certain constant $k$.

Rewrite this as $y=x\tan\theta+kx^2\,\sec^2\theta$, and use the fact that $\sec^2\theta=1+\tan^2\theta$.

We end up with a quadratic equation in the variable $w=\tan\theta$. Solve for $w$, using the Quadratic Formula. Now we have an expression for $\tan\theta$. Apply the $\arctan$ function to get $\theta$.

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    @Miles Rufat-Latre: If you wish, I can solve a specific numerical example. I would have to know *all* the numbers, $g$, initial speed, $x$ and $y$. Now as to why Wolfram Alpha misbehaves, many combinations of the parameters yield no answer. If you throw a javelin with the very slow initial speed of $1$ meter per second, it will never reach the point $(1000,20)$.2011-11-19