The experience presented in this paper is based upon work
with the portable AGA Thermovision thermal-IR camera
equipment in various guises, while flying at low altitudes
in light-to-medium fixed-wing and rotory-wing aircraft
during the past few years.
PRELIMINARY FLIGHT TRIALS IN A LIGHT AIRPLANE
The thermal registrations were made with the AGA Thermo-
vision 750 camera unit (which has a single liquid nitrogen
cooled InSb detector element, in the 5 um band) suspended
within a specially built "photo door", replacing the
standard door of the airplane: a Cessna 185 (Larsson, 1976).
The registrations were made to monitor the local micro-
climate and heat leakage from buildings in dwelling areas
of Uppsala, Sweden. The work was performed at night in
June, at flying heights between 300-1000 m, looking
straight down with the help of a frontsurface mirror
into which the front lens of the horizontally aligned
IR camera was directed.
The experience from these tests can be summed up as
follows:
- It is a practical, technical possibility to register
thermal radiation from the ground and to document its
distribution pattern with the AGA Thermovision 750
mounted in a light airplane. This standard equipment
is easy to handle and requires modest installations
in the plane.Through the use of light airplanes the
operational costs are low.
- The visual, realtime presentation during the flight
gives a very good possibility for detection, thorough
inspection and documentation of IR radiation anomalies
in the area surveyed.
- The detection can be influenced by reflected sunlight
from an object, and not just by the emitted IR radiation.
Registration flights shall thus be performed during
dusk or at night, or alternatively, with an "anti-solar"
filter in the camera.
- The isotherm function of the Thermovision 750 can rarely
be used to an optimum while registration is done from
an airplane, since the objects of interest disappear
so rapidly from the field of view of the downward-
looking camera lens.
- Thermal information is lost from the thermal display image
signals by photographing the screen with a Polaroid-
camera or other photorecording means.
With this experience from the preliminary trials as a back-
ground, some lines of direction for practical operational
flight thermographic activity could be stated: