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Thesis - Leigh Moody.pdf - Bad Request - Cranfield University

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Appendix G / Gravity<br />

_ _<br />

d<br />

−6<br />

2<br />

−8<br />

2 2<br />

( 2 ⋅ λ ) − 3.<br />

2⋅10<br />

⋅ sin λ ⋅ sin ( 2 ⋅ )<br />

∆g<br />

: = − 5.<br />

85⋅10<br />

⋅ sin<br />

λ<br />

GRAVITY ERROR ( micro-g )<br />

0<br />

-10<br />

-20<br />

-30<br />

-40<br />

-50<br />

-60<br />

20-6<br />

d<br />

-70<br />

0 5 10 15 20 25 30<br />

GEODETIC HEIGHT ( KM )<br />

Figure 20-2 : Gravity Error<br />

d<br />

Equation 20.2-16<br />

For short-range applications the geodetic gravitational acceleration in the<br />

Alignment frame is a good approximation to the geodetic value. The LGA<br />

and Alignment frames are closely aligned as the tilt between them over the<br />

distances involved is small.<br />

20.3 Gravitational Anomalies<br />

Figure 20-2 shows the gravitational acceleration error as a function of<br />

geodetic height at 53° latitude if Equation 20.2-6 is used rather than the<br />

more accurate expression in Equation 20.2-5. When doubly integrated over<br />

a long period of time the height error can be substantial, for example, an<br />

error of 2 km is induced at 20 km after 1 hr.<br />

The variation in gravity with geodetic height using the more accurate<br />

expression for the gravitational acceleration,<br />

∂ g<br />

ZG<br />

p<br />

∂ P<br />

ZG<br />

p<br />

For short-range applications,<br />

ZG<br />

p<br />

: =<br />

ZA<br />

p<br />

− 2 ⋅ g<br />

ZG<br />

p<br />

⋅<br />

ZG<br />

p<br />

( ) 1 −<br />

P + P<br />

r,<br />

d<br />

∂ g ∂ P ≅ ∂ g ∂ P<br />

ZG<br />

p<br />

d,<br />

p<br />

Equation 20.3-1<br />

Equation 20.3-2<br />

d

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