An airplane is flying in a horizontal, straight-line path. The speed of the airplane is 100 m/s, and it's altitude is 1000m. What is the rate of change of the angle of elevation, theta, when the horizontal distance from a reference point P on the ground is 2000m?
|dw:1350889896362:dw|
differentiate both sides with respect to time... use the givens (dx/dt = 100 m/s and x=2000m to sub.s in - you'll also need to use x to find the value of theta at that particular moment)
Can you explain what you mean by differntiating both sides? are yousupposed to end up with something like 2x(dx/dt) + (2)2000(dy/dt) = (hypotenuse)?
not really. we don't care about the hypotenuse here. just the angle
\[\frac{ d }{ dt} (\tan \theta = 1000/x)\]
\[\sec^2 \theta \frac{ d \theta }{ dt} = \frac{ -1 }{ x^{2}} \frac{ dx }{dt }\]
dx/dt is given, x is given.... what's theta when x =2000?
\[\sec^2\theta(d \theta/ dt) = -1/4000\] I got this far, but I am confused on how to solve for theta without knowing what dtheta/dt is
you're asked to *find* d(theta) /dt
to do that you'll need to find theta...
pretty easy...:|dw:1350892156875:dw|
RHS should be -1/40000 btw....
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