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6g (4-3 cos)+ sin 20- - sin = 0 (a) Determine the stable and unstable manifolds of the saddle equilibria up to third order.

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6g (4-3 cos)+ sin 20- - sin = 0 (a) Determine the stable and unstable manifolds of the saddle equilibria up to third order. (b)) Consider g = 10 [m/s] and /= 1 [m] and plot the results obtained in part (a). Show that the obtained analytical results correspond to the manifolds obtained by numerical simulations.

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