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

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Chapter 3 / Sensors / Radar Altimeter<br />

_ _<br />

within prescribed limits. A “wide” beam sensor is modelled that can be<br />

characterised as either a continuous wave or a pulsed device whose first<br />

return represents the geodetic ground height. Digital LandMass Survey<br />

(DLMS) map data is used to obtain an estimate of the ground height. The<br />

true ground height is obtained by removing statistical map triangulation and<br />

interpolation height errors from the Digital Terrain Elevation Data (DTED).<br />

The reference height is the difference between the geodetic height above the<br />

earth’s surface and the corrected map height.<br />

REFERENCE<br />

INPUT<br />

1<br />

PZ_GFM<br />

RADALT<br />

ERROR MODEL<br />

3.7-2<br />

M_PZ_GFM I_PZ_GFM<br />

RADAR ALTIMETER<br />

1553 I/F<br />

GUI<br />

1<br />

2<br />

E_PZ_GDM<br />

Figure 3-37 : Radar Altimeter Model<br />

The radar altimeter model does not support narrow beam devices that<br />

require DLMS data at the point of ground impact. When the DTED is deactivated<br />

the geodetic height is referred to the WGS 84 ellipsoid and is thus<br />

comparable with barometric altimeter data.<br />

3.7.2 Reference Height Above the Ground<br />

Since the DTED contains map errors the reference ground height is,<br />

ZG<br />

f , m<br />

G<br />

E<br />

E E G<br />

ZG ZG<br />

( ) P P<br />

~<br />

kˆ P − P • − +<br />

P : = T ⋅<br />

∆<br />

m<br />

d<br />

d,<br />

f<br />

d,<br />

f<br />

Equation 3.7-1<br />

This data is provided at a reference frequency (RAfR) of 400 Hz. The<br />

transform from the Earth to LGA frame, and the Earth radius at point (d)<br />

directly beneath the missile, are defined in §17.10 and §18.3 respectively.<br />

Assuming that the first energy returns represent the geodetic vertical,<br />

~<br />

P : = P − P + ∆P<br />

ZG<br />

f , m<br />

ZG<br />

d,<br />

m<br />

ZG<br />

d,<br />

f<br />

ZG<br />

d,<br />

f<br />

Equation 3.7-2<br />

The measured height of the ground below the missile along the geodetic<br />

vertical is obtained by 3 rd order bi-cubic interpolation between a 4x4<br />

ordinate height patch centred at the missile position, a process described in<br />

§22.6. Whilst transitions between map squares is free from discontinuities,<br />

the mapping and interpolation processes used in generating paper maps and<br />

their digitisation, result in four major errors:<br />

• A zero mean Gaussian height error (∆M1) in metres

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