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

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8 TWO-BODY ORBI TAL MECHANICS Ch.1<br />

F TOTAL = F 9 + F OTHER '<br />

(l.2-6)<br />

We are now ready to apply Newton's second law <strong>of</strong> motion. Thus,<br />

d (mj v j) = FTOTAL. (1.2-7)<br />

The time derivative may be exp<strong>and</strong>ed to<br />

m · dVj dmj_ F<br />

I--+V'--dt<br />

I dt TOTAL<br />

(1.2-8)<br />

It was previously mentioned that the body may be expelling some mass<br />

to produce thrust in which case the second term <strong>of</strong> equation 1.2-8<br />

would not be zero. Certain relativistic effects would also give rise to<br />

changes in the mass m j as a function <strong>of</strong> time. In other words, it is not<br />

always true-especially in space dynamics-that F = ma. Dividing<br />

throur by the mass m j gives the most general equation <strong>of</strong> motion for<br />

the it body<br />

r· =<br />

I<br />

FTOTAL<br />

mj<br />

0.2-9)<br />

whereL-.. ________ .... .. ..I<br />

fj is the vector acceleration <strong>of</strong> the jth body relative to the x, y, z<br />

coordinate system.<br />

mj is the mass <strong>of</strong> the jth body.<br />

FTOTAL<br />

F 9 = -<br />

is the vector sum <strong>of</strong> all gravitational forces<br />

Gmj<br />

n<br />

2:<br />

j = 1<br />

j =1= j<br />

<strong>and</strong> all other external forces<br />

(r .. )<br />

J I

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