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Bate, Mueller, and White - Fundamentals of Astrodynamics ... - UL FGG

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12 TWO-BODY ORBITAL MECHANICS Ch. 1<br />

2. There are no external nor internal forces acting on the system<br />

other than the gravitational forces which act along the line joining the<br />

centers <strong>of</strong> the two bodies.<br />

1.3.2 The Equation <strong>of</strong> Relative Motion. Before we may apply<br />

Newton's second law to deter mine the equation <strong>of</strong> relative motion <strong>of</strong><br />

these two bodies, we must find an inertial (unaccelerated <strong>and</strong><br />

nonrotating) reference fr ame for the purpose <strong>of</strong> measuring the motion<br />

or the lack <strong>of</strong> it. Newton described this inertial reference frame by<br />

saying that it was fixed in absolute space, which "in its own nature,<br />

without relation to anything external, remains always similar <strong>and</strong><br />

irrnnovable."<br />

s However, he failed to indicate how one found this frame<br />

which was absolutely at rest. For the time being, let us carry on with<br />

our investigation <strong>of</strong> the relative motion by assuming that we have found<br />

such an inertial reference frame <strong>and</strong> then later return to a discussion <strong>of</strong><br />

the consequences <strong>of</strong> the fact that in reality all we can ever find is an<br />

"almost" inertial reference frame.<br />

Consider the system <strong>of</strong> two bodies <strong>of</strong> mass M <strong>and</strong> m illustrated in<br />

Figure 1.3-1. Let (X', Y', Z') be an inertial set <strong>of</strong> rectangular cartesian<br />

coordinates. Let (X, Y, Z) be a set <strong>of</strong> nonrotating coordinates parallel<br />

to (X', Y', Z') <strong>and</strong> having an origin coincident with the body <strong>of</strong> mass M.<br />

The position vectors <strong>of</strong> the bodies M <strong>and</strong> m with respect to the set (X',<br />

Y', Z') are rM a nd rm respectively. Note that we have defined<br />

r = r m - rM•<br />

Now we can apply Newton's laws in the inertial frame (X', Y', Z') <strong>and</strong><br />

obtain<br />

- mf = GMm 1..<br />

m<br />

r 2<br />

r<br />

<strong>and</strong> =<br />

Mf<br />

GMm L<br />

M<br />

r 2<br />

r<br />

The above equations may be written:<br />

<strong>and</strong><br />

f m =_-.GMr<br />

r 3<br />

tM= r .<br />

r<br />

(1.3-1)<br />

(1.3-2)

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