Development of a nano-satellite – attitude control system
NTU Satellite Research center initiates the Nano-‐satellite project in 2009 to develop a pico and Nano-‐satellite pair known as VELOX-‐I. Since then, many FYP, URECA and DIP students have been involved in...
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| 主要作者: | |
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| 其他作者: | |
| 格式: | Final Year Project |
| 語言: | English |
| 出版: |
2011
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| 主題: | |
| 在線閱讀: | http://hdl.handle.net/10356/45391 |
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| 機構: | Nanyang Technological University |
| 語言: | English |
| 總結: | NTU
Satellite
Research
center
initiates
the
Nano-‐satellite
project
in
2009
to
develop
a
pico
and
Nano-‐satellite
pair
known
as
VELOX-‐I.
Since
then,
many
FYP,
URECA
and
DIP
students
have
been
involved
in
the
conceptualization,
design
and
prototyping
of
various
subsystems
of
the
nanosatellite.
This
project
is
part
of
the
Attitude
Determination
and
Control
System
(ADCS)
development
work.
The
project
involves
in
the
development
of
a
satellite
attitude
simulator
to
facilitate
the
development
of
the
ADCS.
The
simulator
provides
a
GUI
for
input
the
testing
specifications.
The
simulation
result
base
on
various
environment
and
system
models
will
be
displayed
in
a
3D
animation
video.
The
simulation
of
sensor
data
will
also
be
included
in
the
simulator,
and
the
result
will
be
used
to
test
the
attitude
determination
algorithm
in
the
future
ADCS
projects.
Three
substantial
attitude
control
strategies,
namely
PID,
BDOT,
and
MPC,
have
been
implemented
in
the
simulator
for
test
and
tuning. |
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