1 2004
SS
n
S
DISCREPANCIES BETWEEN OVERLAPPING LASER SCANNER STRIPS -
SIMULTANEOUS FITTING OF AERIAL LASER SCANNER STRIPS
H. Kager
Vienna University of Technology,Institute of Photogrammetry and Remote Sensing,
Gusshausstr. 27-29 / 122, A-1040 Wien, hk@ipf.tuwien.ac.at
Commission II, WG II[/1
KEY WORDS: Adjustment, Calibration, Orientation, DEM/DTM, Laser scanning, Gps/Ins, Georeferencing, Reliability
ABSTRACT:
This paper deals about discrepancies between overlapping laser scanner strips. We assume these discrepancies stemming from non-
sufficient system calibration. These discrepancies - in height as well as in planimetry - are unsatisfactory phenomena for end-users
of the ground data. Nevertheless, these gaps can be eliminated to a great portion doing a simultaneous 3D adjustment by least
squares. An adjustment strategy is proposed for doing that: correcting those exterior orientation elements as recorded by dGPS and
IMU, as well as interior orientation elements concerning the Scanner-dGPS-IMU system. The method (functional model) chosen is
to apply correction polynomials in the time domain to all degrees of freedom as determined by the dGPS-IMU components and to
the relative orientation parameters between those scanner-system components. All these parameters may be chosen block- or strip-
variant and are determined simultaneously with hybrid adjustment by least squares. "Preventive regularisation" is used to catch un-
or weakly determinable parameters. Automated determination (measurement) of tie features (instead of tie points) is described.
Since in the point-clouds no corresponding points can be found, tying features - as planes and straight lines as their intersection - are
used. Noise (e.g.) from the cover of vegetation has to be considered in this context; so, homologous point-clusters with low noise
and few exceptions with respect to an adjusting plane have to be searched for. Speaking in the terms of standard photogrammetry,
"homologous planes" replace "homologous points" as tying features in block adjustment of strips as unit; "strips" replace "photos" or
"models". Nevertheless, an originally photogrammetric adjustment programme could be successfully extended to perform the task.
Once, this programme had also been extended to handle scanner images, introducing time dependent parameters. The history of
evolution of the mathematical model reveals the strong relationship between laser scanning and photogrammetry and geodesy. The
distribution of control features (instead of control points) is discussed. Colour-coded difference-DEMs are used to judge the
improvement of interior and exterior orientation.
1. INTRODUCTION
For transforming laser scanner strips into the national ground-
1.1 General
Laser scanners are mounted in aircrafts for collecting 3D-data
of the surface of the earth. Proceeding the flight path, the laser
beam sent downwards is deflected rhythmically aside and scans
the ground surface in a meandric or parallel pattern with a high
pulse rate. Most such devices use the technique of run-time
measurement: the distance to a ground point then is a function
of the time gap between the pulse was sent and received.
The direction of the laser beam is given by some deflecting
device like a rotating or oscillating mirror and some trigger
causing discrete pulses. So, the device records polar co-
ordinates of ground points in its own local co-ordinate system.
The origin of this device co-ordinate system follows the flight
path and its movement can be measured with dGPS (differential
Global Positioning System) very precisely using the phase
comparison method. Since coupled to the aircraft, the attitude
of the device changes also during the flight and can be recorded
with INS (Inertial Navigation System) — more exactly spoken,
with an IMU (Inertial Measurement Unit).
The components GPS, IMU and laser scanner have to be
synchronised; moreover, their relative - but constant -
displacements have to be determined (calibration of
eccentricities).
555
survey co-ordinate system using dGPS and INS, we principally
need only one ground reference station with known ground-
survey coordinates. Moreover, we need also the form of the
geoid. But, in practice, we should not be satisfied with that
minimal solution because:
e The form of the geoid is not sufficiently ( up to some few
cm ) known in many regions.
e The on-the-fly-initialisation for solving the GPS phase
ambiguities nowadays is possible for fast moving objects
like aircrafts with a r.m.s.e. of about 10cm; this might
result in errors of some dm. Usually, neighbouring
precision of dGPS is better by one order of magnitude. The
errors increase with the strip length. (Cramer, 2000)
e The attitudes as delivered from IMUs in use are prone to
errors of about 0.01gon resulting in 16cm on the ground
assuming 1000m relative flying height. Errors of IMU
attitude also introduce some torsion of the laser scanner
strips inducing errors in ground coordinates. Alike, IMU
attitudes have a high neighbouring precision based on the
gyros used; nevertheless, they show drifting phenomena.
The resulting error effects might reach again some dm in
the positions of ground points. (Cramer, 2000)
e System failure or system instabilities shall be mentioned
also: e.g. the change of the set of available GPS satellites