fired vertically upwards and allowed to fall back
along the same path. The gravity measurement
depends on timing the upward and downward paths,
which may be by light beam-controlled timers or
interferometry.
Gravity differences can be measured on land with a
stable gravity meter or gravimeter based on Hooke’s
law. A mass extends a spring under the influence of
gravity and changes in extension are proportional to
changes in the gravitational acceleration. More sensi-
tive are ‘astatic’ gravity meters, which contain a mass
supported by a ‘zero-length’ spring for which tension
is proportional to extension. When the meter is in
position, a measurement is made of an additional
force needed to restore the mass to a standard pos-
ition, supplied by an auxiliary spring or springs, an
electrostatic system, or an adjustment of the zero-
length spring itself. Gravity meters working on this
principle measure differences in gravity between sta-
tions and surveys may be tied to one or more base
stations at which repeated measurement can be made.
Astatic gravity meters can have a sensitivity of about
0.01 mGal.
For applications where the gravity meter is sub-
ject to tilting and vibration, such as on board a ship
or in an aircraft, isolation of the instrument is re-
quired such as providing a moving stabilised plat-
form for the gravity meter and damping vibrations
with appropriate shock absorption. When the gravity
meter is moving, accurate data on the location and
trajectory of the platform is required along with
the gravity measurement. For airborne application,
this requirement has been greatly assisted by the
advent of the global positioning system (GPS) which
allows rapid, precise, and accurate positioning (see
Remote Sensing: GIS). Airborne gravity surveys,
whether flown using fixed wing or helicopters, can
provide economic, rapid, and non-invasive geophys-
ical reconnaissance ideal for difficult terrain such as
tundra, jungles, and wildlife reserves.
Deviations in artificial satellite orbits can be used
to determine the long-wavelength components of the
Earth’s gravity field. Altimetry tools mounted on sat-
ellites have allowed much more detailed gravity map-
ping over the oceans, as sea surface height data can
be processed to give the marine geoid. Geoid data
can then be converted to gravity data with a series
of numerical operations (Figure 2). Since the mean
sea-level surface is the geoid, an equipotential surface,
variations in sea surface height from the reference
ellipsoid reflect density changes below the sea surface,
largely from the density contrast at the seabed,
but also from sub-seabed changes, such as crustal
thickness changes.
Adjustments to Measured
Gravity Signals
The first correction that can be applied to measured
gravity values is the correction for latitude, to account
for the centrifugal acceleration which is maximum
at the equator and zero at the poles (Table 1). For
gravity measurements made on land, several further
corrections must be made (Table 1). The ‘free-air cor-
rection’ is made to adjust for difference in height be-
tween the measurement point and sea-level. This does
not make any assumptions about the material between
the sea-level datum level and the observation point and
uses the inverse square law and the assumption of a
spherical Earth. The ‘Bouguer correction’, named after
the French mathematician and astronomer, is used to
account for the gravitational effect of the mass of ma-
terial between measurement point and sea-level. This
requires assumptions to be made about the density of
material, and the Bouguer plate or slab formula is
applied (Table 1), which further assumes that this ma-
terial is a uniform infinite plate. Historically a ‘density
correction’ value of 2670 kg m
3
has been used as a
standard density for crustal material, and this corres-
ponds to a Bouguer correction of 1.112 g.u./m, nega-
tive above sea-level. A ‘terrain correction’ may be
applied to compensate for the effect of topography,
again requiring assumptions about densities. Nearby
mass above the gravity measurement station will de-
crease the reading and any nearby topographic lows
will have been be artificially ‘filled in’ by the Bouguer
correction so the correction is always positive. An add-
itional correction to gravity measurements made on a
moving vehicle such as an aeroplane or boat is the
Eo
¨
tvo
¨
s correction, which depends on horizontal speed
vector, latitude, and flight altitude.
Gravity Anomalies and Derivatives
Since for most geological applications the perturb-
ations in the gravity field across an area or feature
of interest are more important than the absolute grav-
ity values, it is standard to compute gravity anomalies
by subtracting the theoretical gravity value from the
observed. The Bouguer gravity anomaly is the ob-
served value of gravity minus the theoretical gravity
value for a particular latitude and altitude, as outlined
in Table 1. The Bouguer gravity is commonly used on
land where maps of gravity anomalies can be used to
view gravity data in plane view and it is convenient to
have topographic effects (approximately) removed.
Offshore, the free-air gravity anomaly is most useful,
as the measurements are straightforward to correct to
the sea-level datum.
ANALYTICAL METHODS/Gravity 95