Nothing Special   »   [go: up one dir, main page]

Cansat Development Program in Tokyo Institute of Technology

Download as pdf or txt
Download as pdf or txt
You are on page 1of 16

CanSat Development

Program in Tokyo Institute of


Technology

International CanSat Workshop


2007
Tokyo Institute of Technology Matunaga Lab.
Yasumi Konda
Contents
Introduction
CanSat projects in Tokyo Tech
„ Image acquisition
„ ComeBack competition
„ Demonstration of CubeSat’s function
„ Educational aspect
ComeBack Competition in Japan
Future perspectives

International CanSat Workshop 2007


Introduction
We develop our CanSats around four main objectives..
Image acquisition
„ Main objective : to Have fun!!
„ … and to use the pictures as confirmation for other missions
ComeBack competition
Basic experiments for space application
For example we conducted an antenna deployment
experiment in 2001 and then used this knowledge for our
CubeSat.
Educational purposes
New members who have not joined the CubeSat project yet
gain knowledge through the CanSat projects. After
completion, they are integrated in the CubeSat development
team and entrusted with some main tasks.

International CanSat Workshop 2007


CanSats of Tokyo Tech
Tokyo Tech members have developed 22 CanSats !
We have participated in Arliss in Nevada since 1999
,Itakura Competition in 2002 and 2003
,Kyusyu Competition in 2004 and 2005
and Noshiro Competition in 2005 and 2006
1999 Spider
Tether mission
Tether Shuttle
Tether mission
[etc.]
Data acquisition
SabSat
Image acquisition
Yellow:
2000 C4-SAT AQUARIUS GNSSAT SabSat2 SSTV-SAT OpenClass size
Image acquisition Data acquisition GPS mission Image acquisition SSTV mission
2001 OpenClass SabSat3 (8 CanSats)
ComeBack Image acquisition
2002 OpenClass CanSat GEMINI
Rover mission ComeBack ComeBack
2003 CUTEii Tracky by the
ComeBack ComeBack
2004 Pelican MAEDA Monster members who
ComeBack
2005 Tomas
New Technology
Mo-Sat
ComeBack are 3rd year
Image acquisition ComeBack students at
2006 Da Vinci Spopovic
ComeBack ComeBack Tokyo Tech

International CanSat Workshop 2007


Image acquisition(1)
1999 ATV 1200MHz 2000

The 1st year, we simply put an


Amateur TeleVision (ATV) equipment
In 2000, with a higher transmission
set on the CanSat like on the right
power, we succeeded in the
figure.
acquisition of images of much
The image acquired by the camera is
better quality.
shown in the left but it is not good
because the power transmission is
very limited
This technology can be applied for other missions in order to monitor a mechanism
working. For example, in 2001, to monitor antenna deployment mechanism, this
movie transmitting system was used. And in 2003, the parafoil deployment
mechanism was also monitored by the camera and the movie transmitted by radio.

International CanSat Workshop 2007


Image acquisition(2)
2004 2005

The team installed a film camera The team installed a common


on the CanSat to take more digital camera on the CanSat to
beautiful pictures from the sky. take high resolution pictures.
Two motors handled the camera,
one for sliding and the other for An onboard computer using Linux
pushing the shutter button. controlled the triggering of the
The results were good but capture, using a remote USB PTP
slightly blurred since this camera protocol. 36 high resolution
didn’t have integrated shutter pictures were taken in the air.
speed control.
These experiments were fun.
International CanSat Workshop 2007
ComeBack competition(1)
This project started in 2001 when the
members of Matunaga Lab. developed a first
CanSat for the ComeBack competition.
2001 In this first CanSat, we controled
the parafoil to come back to the
OBC target point using GPS data.
Battery
Battery
This mission however failed
because the strong force due to
GPS Receiver Servo Motor the rapid deployment of the
injured the motor shortly after
ejection from the rocket.
International CanSat Workshop 2007
Come back competition(2)
2002 2003

By using two motors, we We tried to conduct an


tried to prevent the experiment of a two-step
destruction of the motor
To prevent
spiral motion deployment using a parachute
as in 2001. This problem and parafoil. We considered that
was indeed solved but a after ejection
it would make the CanSat’s
new problem came up from the rocket: attitude more stable.
…spiral motion, This experiment however failed
caused by a deficient because the structure was too
deployment of the parafoil. weak and broke.

International CanSat Workshop 2007


Technology Demonstration
CanSat -- Satellite
Similarities
CanSat can be considered as a good experimental model for satellites
because they are thrown away from a rocket that might shake it hard,
and during all the mission process physical interation is impossible
with it.
Differences
One of the differences is that a CanSat can be picked up after the
experiment is over.

We think it is significant to conduct on CanSats verification


experiments of technology which will be used for CubeSat or
other satellites.
International CanSat Workshop 2007
Demonstration(1)
Antenna deployment
We conducted an
2001 Antenna antenna deployment
for camera Nichrome line
mechanism experiment
for our 1st CubeSat,
Deployment
CCD camera CUTE-I.
Structure Antenna

In the left figure, three flexible antennas are originally coiled and tied with Nylon
line. In the air, the Nylon line is cut using heat and the three antennas are
deployed. This mechanism was going to be installed in the CubeSat. The
verification test on the CanSat was monitored by an ATV camera which had been
developed since the 1st CanSat experiment in 1999.

After the CanSat was launched, the movie taken by camera was downloaded
on our screens in real time, using an FM transmitter, and we are informed of
the experiment’s success.
Our first CubeSat CUTE-I was launched in 2003, using this antenna
deployment mechanism and was a success in space thanks to our previous
CanSat expriment
International CanSat Workshop 2007
Demonstration(2)
GMSK experiment
2004
we conducted in 2004 another
verification mission for our second
CubeSat, named “Cute-1.7 +
APD”.
In this mission:
We tested the GMSK modulation, which is a better modulation than the
classic one, and checked our system. The GMSK modem for CubeSats was
developed to enable higher rate communications in order to transfer larger
image files.

That experiment wasn’t a full success, but we acquired useful knowledge.


After some improvements were made to the modem, the Cute-1.7 + APD
Cubesat was launched with this system and was able to communicate with
the ground station from space using GMSK modulation.

International CanSat Workshop 2007


Training of 3rd year students
Since the CanSat project has educational aspects, it’s good for our university
students in engineering course to have an experience in CanSat development
when they are in their third year.
We thus train students highly interested and eager to work students.
This is also a part of the appeal of our laboratory, and we can thus expect
members with experience gained in this project to join us.
In 2003, we started this scheme for the first time in Japan, and 6 members
developed a CanSat during their 2 month summer vacation.

GPS Antenna
OBC
Servo Motor

Transceiver
Circuit Board Antenna

We were pleased to see that many of those who took part in the
CanSat project when they were in 3rd year then joined the
Matunaga Laboratory !
International CanSat Workshop 2007
Training of new laboratory members
2005 2006 ・ComeBack
・Linux
・Digital Camera ・GMSK
・2.4GHz ATV
All five members Four members
were new out of six were
members of the new members.
laboratory

These days, the CanSat projects provide the new members of


Matunaga Lab. with an on-hand experience. These CanSats are
developed by students who do not know much about satellite
development, but want to have an experience.
This is a part of educational activities where, while making a CanSat,
they learn a lot not only about satellite development but also the
importance of teamwork and project planning.
They are now mostly members of the CubeSat project.
International CanSat Workshop 2007
Competitions in Japan
2004,2005 2005,2006 Apart from ARLISS, we have also
taken part in all the competitions
held in Japan as shown the left
figure. We could fix some CanSats
by learning from the failures
during ARLISS and try again using
balloon instead of rockets launches
in Itakura and Kyusyu.
In 2005 the competition at Noshiro
started.

2002,2003
International CanSat Workshop 2007
Future perspectives
Education 2005
„ Learn about satellite development Tomas

„ Learn about the importance of teamwork and


project planning
Appeal
„ To interest the members who didn’t belong
previously to the Matunaga Lab. 2004 Monster

Demonstration opportunity for new


technologies looking forward to
„ CubeSat project
„ …and other space missions
2001 OpenClass

International CanSat Workshop 2007


Thank you for your attention.

http://lss.mes.titech.ac.jp/ssp/arliss/

If you have any question don’t hesitate to


contact us at
yasu@lss.mes.titech.ac.jp

International CanSat Workshop 2007

You might also like