2011 - Cooperative Institute for Research in Environmental Sciences ...
2011 - Cooperative Institute for Research in Environmental Sciences ...
2011 - Cooperative Institute for Research in Environmental Sciences ...
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Ben Balsley<br />
F<strong>in</strong>e-Scale In Situ Measurements to Study<br />
Atmospheric Dynamics (0-10 km)<br />
We are currently <strong>in</strong>volved<br />
<strong>in</strong> exam<strong>in</strong><strong>in</strong>g the<br />
f<strong>in</strong>e-scale details of atmospheric<br />
dynamic processes<br />
from the surface<br />
to upper-tropospheric<br />
heights. Understand<strong>in</strong>g<br />
these processes, which<br />
occur on scales of meters<br />
and seconds, is turn<strong>in</strong>g<br />
out to be critical <strong>for</strong> ga<strong>in</strong><strong>in</strong>g<br />
a better understand<strong>in</strong>g<br />
of energy-cascad<strong>in</strong>g<br />
processes throughout<br />
this region.<br />
The vehicle used <strong>in</strong><br />
these measurements,<br />
called the CUMAV<br />
(University of Colorado<br />
Micro Autonomous<br />
Vehicle), was developed by Professor Dale Lawrence of<br />
CU’s Aerospace Eng<strong>in</strong>eer<strong>in</strong>g Department. The CUMAV<br />
is a small, low-cost, programmable, reusable, autonomous,<br />
GPS-controlled, battery-powered aircraft. Total cost<br />
per unit is <strong>in</strong> the vic<strong>in</strong>ity of $1,000. CIRES has equipped<br />
it with fast-response sensors to measure temperature,<br />
humidity, w<strong>in</strong>d speed, w<strong>in</strong>d direction and ‘temperature’<br />
turbulence (CT2). Data are both telemetered to the ground<br />
as well as archived aboard <strong>for</strong> later download<strong>in</strong>g and<br />
analysis.<br />
For upper-tropospheric measurements, the CUMAV<br />
will be carried aloft beneath a conventional meteorological<br />
balloon. After release, it will fly to a specific location,<br />
spiral downward and then land at a predeterm<strong>in</strong>ed site.<br />
Typical spiral diameter is 100 to 200 m. Vertical resolution<br />
is <strong>in</strong> the range of 1 to 2 m.<br />
An example of our <strong>in</strong>itial measurements appears <strong>in</strong><br />
Figure 1. This figure plots temperature (expressed here<br />
<strong>in</strong> volts) versus time. These data were obta<strong>in</strong>ed while<br />
the CUMAV was fly<strong>in</strong>g a series of 12 circles at a constant<br />
height of 56 m over central Kansas. Although the<br />
full range of temperatures shown here is very small<br />
(1.11–1.17°C), a clear <strong>in</strong>dication of mean heat<strong>in</strong>g can be<br />
seen by the upward trend <strong>in</strong> the dotted l<strong>in</strong>e. The sharp<br />
‘spikes’ on top of this mean curve appear to be manifestations<br />
of early convective activity that <strong>in</strong>creases with time<br />
as the atmosphere warms. The horizontal width of the<br />
smaller spikes can be less than 15 m or so.<br />
We anticipate that this technique will serve as an impetus<br />
<strong>for</strong> develop<strong>in</strong>g a unique, new and powerful technology<br />
<strong>for</strong> study<strong>in</strong>g f<strong>in</strong>e-scale dynamic processes throughout<br />
the first 10 km of the atmosphere.<br />
PHOTOS BY DAVID OONK/CIRES<br />
In one of three possible launch modes, the CUMAV is launched us<strong>in</strong>g a bungee<br />
cord. In this case, the actual release is triggered by a computer command.<br />
Dale Lawrence, Professor Aerospace Eng<strong>in</strong>eer<strong>in</strong>g <strong>Sciences</strong>, prepares to<br />
launch the CUMAV by hand.<br />
To launch from a higher altitude, the CUMAV is raised <strong>in</strong>to the air via balloon,<br />
released and then controlled remotely. Land<strong>in</strong>g the CUMAV <strong>in</strong> all situations<br />
is autonomous, with the land<strong>in</strong>g site programmed prior to launch.<br />
Because of its relative ruggedness (Styrofoam fuselage, pusher propeller<br />
and embedded sensors), the aircraft can land safely virtually anywhere.<br />
Figure 1<br />
CIRES Annual Report <strong>2011</strong> 25