Yamaha Motor Co., Ltd., at the request
of the Public Works Research Institute of the Ministry
of Construction of Japan, has begun conducting autonomous-flight
observation of topographical and geological conditions
in the area around Mt. Usu in Hokkaido using a Yamaha
industrial-use unmanned helicopter equipped with GPS
and, video and still cameras. Volcanic activity has
continued at a high level since Mt. Usu's eruption earlier
this month and flight by manned aircraft is presently
under restriction.
This is the first autonomous-flight observation project
of its type ever undertaken in Japan, and possibly in
the world. Autonomous flight systems are presently under
development at universities and research organizations
around the world, but this represents the first time
that such a system has been put to practical use out
of the visual range of the operators. |
|
Since April 20, a team of employees
from Yamaha's Aeronautic Operations has been on the
scene in Hokkaido with a Yamaha helicopter specially
outfitted for observation purposes. They have been conducting
observation flights under the supervision of a team
specializing in landslide measures. The observation
flights are mainly surveying the area around the Itaya
River to provide information for mudslide measures.
In the Mt. Usu area, mudslides resulting from the volcanic
ash build-up from the volcanic eruption have already
been observed. And, as the volcanic activity in the
area continues, it is feared that large-scale mudslides
are imminent. It is hoped that an autonomous-flight
unmanned helicopter to observe the build-up of volcanic
ash and boulders and other volcanic projectiles will
add to the accuracy of data available for giving warnings
or considering preventative measures against mudslides
and landslides. These unmanned-autonomous-flights are
being conducted in areas where manned flight presently
is prohibited.
The basic helicopter being used for these flights is
the industrial-use unmanned helicopter Yamaha Aero Robot
"RMAX," which is normally operated by remote control
within the operator's range of vision. To accommodate
the long-distance flights necessary for the observation
work at the volcano sight, a GPS system and control
box is mounted on the helicopter to enable use of an
autonomous-flight program. This and other modifications
made it possible to completely automate flight over
the roughly 4-kilometer round trip from the observation
center to the volcano and around the survey area. Also,
an auxiliary fuel tank was added to extend the continuous-flight
capability to one hour or more, and other special equipment
such as auxiliary remote control capacity was employed
as well. For the helicopter's observation function a
video and a still cameras are mounted along with three
small-size cameras for navigational purposes. Images
from these cameras are sent from the helicopter to the
control center on a real-time basis, where they are
viewed on a four-window spilt screen monitor. |
|
|
Comment from
Senior General Manager Kazuo Uchiyama, Yamaha Aeronautic
Operations |
|
|
"This is the first time not just for
us but in the history of Japanese disaster management
that an autonomous-flight helicopter has been used for
observation operations. The unmanned helicopter makes
it possible to conduct observation activities in areas
too dangerous for manned flight, but we came prepared
for the fact that the flights would be conducted under
very harsh conditions around the erupting Mt. Usu, including
not only volcanic ash, flying rocks and other projectiles
thrown up by the volcano but also highly unstable air
flows and high temperatures. Up until this point the
observation flights have been even more effective than
we expected and we hope to continue collecting visual
data that will contribute to the disaster relief and
prevention measures." |
|
|
Reference |
|
|
Main specifications
for the autonomous-flight GPS helicopter (RMAX-base) |
HELICOPTER |
Main rotor diameter |
: |
3,115 mm |
Tail rotor diameter |
: |
545 mm |
Overall length |
: |
3,630 mm (including
rotor) |
Overall width |
: |
800 mm |
Overall height |
: |
1,220 mm |
Operating weight |
: |
Approx. 95 kg |
ENGINE |
|
|
Type |
: |
Liquid-cooled 2-stroke horizontal
opposed-type |
Displacement |
: |
246cc |
Power output |
: |
21PS |
Starting system |
: |
Electric start |
Fuel |
: |
Gasoline-oil mixture |
PERFORMANCE |
|
|
Max. flying time |
: |
60 min. (with standard 6 liters
fuel tank)
100 min.(with standard 6 liters fuel tank plus
5 liters auxiliary fuel tank) |
Flight speed |
: |
15 to 20 km/h |
Flight height |
: |
Ground height 30 to 150 m |
Photographing equipment |
: |
Video camera Single-lens reflex
camera |
|
|