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International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences, Vol XXXV, Part B3. Istanbul 2004
3.4 Radar Equation
The intensity of the received laser pulse can be determined from
the range equation, which describes the influences of sensor,
target, and atmosphere (Jelalian, 1992):
pp
2 m : i 2 : Toys ai GE Ch
4zR' ff;
where P, — received signal power (watt)
P, — transmitted signal power (watt)
D, — diameter of receiver aperture (meter)
R — range from sensor to target (meter)
f= laser beamwidth (radian)
Mss = System transmission factor
Num = atmospheric transmission factor
o = target cross section (square meters)
The radar equation shows that the received power is a function
of transmitter power, laser beamwidth, aperture size of the
receiver, system losses, and atmospheric transmission. The
properties of the target are described by a single quantity, the
backscattering cross section.
The backscattering cross section is, as its name suggest, the
effective area for collision of the laser beam and the target,
taking into account the directionality and strength of the
reflection (Jelalian, 1992). Therefore it has a unit of square
meters. In the case of airborne laser scanning the wavelength is
always much smaller than the size of the scattering elements
(e.g. leaf, roof). Therefore, the effective area for collision is
simply the size of the projected area of the scatterer. The
magnitude and directionality of the reflected energy depends
strongly on the surface properties of the target and its
orientation with respect to the incoming beam.
3.2 Pulse Form
Models which are capable of simulating the waveform from
different targets are already available. For example, Sun and
Ranson (2000) present a model for forest canopies which
assumes that laser scanners are working on a hot spot condition
(because the light source and detector are at the same point).
Here we build upon the radar equation, noting that in the way as
it is written in equation (1) it only applies for point scatterers or
non-tilted surfaces. In case of distributed targets, where
scattering of the incoming laser beam takes place within the
range interval [R;, R,], the return-signal strength is the
superposition of echoes from portions of the target at different
ranges (Ulaby et al, 1981). Mathematically, this can be
expressed by an integral:
R 2
nbi 2R
P()= |— 177 ssn" B| 1 —— | o(R)dR (
AzR' fi y
t g
N
)
where f is the time, v, is the group velocity of the laser pulse,
and o(R)dR is the differential backscattering cross section do in
the interval dR (Wagner et al., 2004). The group velocity v, for
optical and near-infrared radiation in dry air differs from the
speed of light in vacuum by at most 0.03 % (Rees, 2001), so
here we use v, « 3-105 ms. The term 2R/v, in the brackets is
the round trip time.
It must be considered that at range R some scattering elements
may be shaded by objects situated above this range, i.e. in the
interval [R,, R]. Since these shaded areas do not contribute to
the return signal, do represents an "effective" or “apparent”
cross section that represents only illuminated scatterers in dR.
As an example, lets us consider the ground surface beneath a
tree. If 90 % of the ground surface is shaded by leaves and
branches, then the “effective” cross section of the ground is
10 % of its actual cross section.
In the next section we will study the impact of different pulse
detection methods on the distance measurements. For this
purpose it is sufficient, in a first step, to focus solely on the
waveform of the return pulse. In more advanced studies also the
different parameters which modulate the signal strength should
be considered.
4 IMPACTS OF PULSE DETECTION
4.1 Detection Methods
Pulse detection is applied on the backscattered waveform. The
task of the detector is to derive from the continuous waveform
discrete, time-stamped /rigger-pulses, which encode the
position of the individual targets, thus allowing to compute the
distance between the scanner system and the generator of the
return pulses, i.e., the illuminated objects. Since the details of
detection methods applied by commercial laser scanner systems
are currently not known, we will consider here a number of
standard detection methods: threshold, centre of gravity,
maximum, zero crossing of the second derivative, and constant
fraction.
The most basic technique for pulse detection is to trigger a
pulse whenever the rising edge of the signal exceeds a given
threshold (Figure 1); although conceptually simple and easy to
implement, this approach suffers from a serious drawback: the
position of the triggered pulse (and thus the accuracy of any
distance measurements derived from it) is rather sensitive to the
amplitude and width of the signal. The same holds for the
centre of gravity when computed over all points above a fixed
threshold. More sophisticated schemes are based on finite
differences respectively numerical derivatives — e.g. the
detection of local maxima or the zero crossings of the second
derivative — or, more generally, the zero-crossings of a linear
combination of time-shifted versions of the signal. An example
of the latter approach is the constant fraction discriminator,
which determines the zero crossings of the difference between
an attenuated and a time delayed version of the signal.
Maximum, zero crossing, and constant fraction are invariant
with respect to amplitude variations and, to some degree, also
changes in pulse width. In practice, these detectors should only
trigger for signal amplitudes above a given threshold (this
"internal" threshold is not to be confused with the threshold
detector) in order to suppress false positives, i.e. spurious
trigger-pulses due to noise. This is especially true for operators
based on higher order derivatives like zero crossing, which are
known to be rather noise-sensitive.
Figure 2 illustrates the trigger-pulses generated by the five
detectors discussed above for the case of a single mode return
signal from rough terrain, assuming a Gaussian differential