Equations (11.41)–(11.43) and (11.47)–(11.49) yield
It is also easily demonstrated thatThe Cartesian components of the lunar equation of motion, (11.33), are
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(11.54) |
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(11.55) |
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(11.56) |
It is convenient, at this stage, to adopt the following normalization scheme:
with![]() |
(11.75) |
Equations (11.62)–(11.65) and (11.69)–(11.71) yield
Likewise, (11.62)–(11.65) and (11.72)–(11.74) give![]() |
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|
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||
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(11.80) | |
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|
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||
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(11.81) | |
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(11.82) |
Finally, let us write
Here,![]() |
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(11.89) |
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|
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||
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||
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||
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(11.90) | |
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|
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||
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(11.91) | |
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(11.92) | |
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(11.93) |
After Equations (11.86)–(11.93) have been solved for ,
,
, and
, the geocentric Cartesian coordinates, (
,
,
), of the Moon in the
non-rotating reference
frame are obtained from Equations (11.44)–(11.46), (11.60)–(11.61), and (11.83)–(11.85). However, it is more convenient to write
,
, and
, where
is the radial distance between the Earth and Moon, and
and
are termed the Moon's geocentric (i.e., centered on the Earth) ecliptic
longitude and ecliptic latitude, respectively. Moreover, it is easily seen that, neglecting terms that are third order, or greater, in the small parameters
,
,
, and
,