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

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4<br />

LF=m r<br />

TWO-BODY ORBITAL MECHANICS<br />

,<br />

,<br />

,<br />

,<br />

,<br />

"<br />

I<br />

I<br />

I<br />

,<br />

I<br />

,<br />

I<br />

, /<br />

, /<br />

- -- -'V<br />

Figure 1.1-1 Newton's Law <strong>of</strong> Motion<br />

y<br />

Ch. 1<br />

(Ll-1)<br />

where LF is the vector sum <strong>of</strong> all the forces acting on the mass m <strong>and</strong> r<br />

is the vector acceleration <strong>of</strong> the mass measured relative to an inertial<br />

referenc e frame shown as )0(Z in Figure 1.1-1. Note that equation<br />

(1.1-1) applies only for a fixed mass system.<br />

1.1.3 Newton's Law <strong>of</strong> Universal Gravitation. Besides enunciating<br />

his three laws <strong>of</strong> motion in the Principia, Newton fo nnulated the law <strong>of</strong><br />

gravity by stating that any two bodies attract one another with a force<br />

proportional to the product <strong>of</strong> their masses <strong>and</strong> inversely proportional<br />

to the square <strong>of</strong> the distance between them. We can express this law<br />

mathematically in vector notation as:<br />

Fg = - GMm r<br />

r 2 r<br />

(1.1-2)<br />

where F 9 is the force on mass m due to mass M <strong>and</strong> r is the vector from<br />

M to m. The universal gravitational constant, G, has the value<br />

6.67Ox10-8 dyne cm2 Igm2 •<br />

In the next sections we will apply equation (1.1-2) to equati ;n<br />

(1.1-1) <strong>and</strong> develop the equation <strong>of</strong> motion for planets <strong>and</strong> satellites.

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