Path of a projectile traveling along a meridian of the earth

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SUMMARY

The discussion focuses on the mathematical modeling of a projectile's trajectory along a meridian of the Earth, as outlined in "Advanced Engineering Mathematics" by E. Kreszig. The path is defined by the vector equation \(\vec{r(t)}=R\cos(\gamma t)\vec{b} + R\sin(\gamma t)\vec{k}\), where \(\vec{b}\) represents the horizontal motion. The acceleration vector \(\vec{a(t)}\) is derived through differentiation, yielding terms for centripetal and Coriolis accelerations, with the third term representing the z-component of centripetal acceleration. The discussion highlights the importance of correctly identifying these components in projectile motion analysis.

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Homework Statement


I've been working out an example by myself from the book Adv. Engg. Mathematics, E.Kreszig, section 8.7 p441.

The path of a projectile traveling along a meridian of the Earth uniformly may be given by
[tex]\vec{r(t)}=Rcos\gamma t\vec{b} + Rsin\gamma t\vec{k}[/tex] where i,j,k are unit vectors along x,y,z axes respectively.

The vector [tex]\vec{b}[/tex] is defined as [tex]\vec{b}=cos\omega t\vec{i} +sin\omega t\vec{j}[/tex]

Differentiating [tex]\vec{r(t)}[/tex] twice to get the expression for acceleration. This comes out to be

[tex]\vec{a(t)}=-R(\gamma ^2+\omega ^2)cos(\gamma t)\vec{b} -2R\gamma sin(\gamma t)\vec{b'} - R\gamma ^2cos(\gamma t)\vec{k}[/tex].

The first term is the centripetal acceleration due to the Earth and the path of the projectile, the second is the coriolis acceleration. What is the third term?
 
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It is the z component of the centripetal acceleration.
It should have sin\gamma t.
 
Oh. ! thank you. That was incredibly stupid of me.
 

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