378(3): Initial Condition Method

This is the initial condition method for aether engineering an orbit, using the general result (3) for any orbit from the field equations. The orbit will depend on the values chosen for the initial kappa vector components.The ratio of kappa sub X(0) and kappa sub Y(0) is a constant input parameter. Then the force component equations are solved simultaneously for this initial condition.

a378thpapernotes3.pdf


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