授課老師:
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SPACE
SYSTEM ENGINEERING
(Class Time: Every Thursday evening 6:00 to 8:30pm)
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Topic
1 : SIntroduction to satellite system in general, picosat
in particular.
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Teacher
: 莊哲男老師(Prof. Jer-Nan Juang)
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Period:
1 weel
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Topic
2: Mission design and requirements Instructor
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Teacher:
莊哲男老師(Prof. Jer-Nan Juang)
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Period:
1 week |
| Topic
3: Payload analysis and orbit design |
Teacher:
莊哲男老師(Prof. Jer-Nan Juang) |
Period:
1 week |
| Topic
4: Power system |
Teacher:
莊哲男老師(Prof. Jyh-Ching Juang) |
Period:
1 week |
| Topic
5: 1. Introduction to project review procedure and期中&期末報告
requirements,2. Software introduction including STK, Matlab,3.
Introduction to Orbit and power analysis. |
Teacher:祝飛鴻老師
(Prof. Chyanbin Hwu) |
Period:
1 week |
| Topic
6: Configuration and Structural DesignInstructor |
Teacher:
胡潛濱老師 (Prof. Y. Y. Lin) |
Period:
1week |
| Topic
7: Attitude determination and controlInstructor |
Teacher:
林穎裕老師 (Prof. Jung-Hua Chou) |
Period:
2 week |
| Topic
8: Thermal control |
Teacher:
周榮華老師 (Prof. Marco Yeh) |
Period:
2 week |
| Topic
9: Telemetry and telecommunication |
Teacher:
莊智清老師 (Prof. Yei-Chin Chao) |
Period:
2 week |
課程設計:
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SPACE SYSTEM ENGINEERING
Rationale
on PicoSat course design:
Supplement to the course outline attached,
this two-page document is to elaborate the idea for the design
of the course, which also incorporates Dr. Chu's opinion on 7
July 2003.
1. Goal of the course:
The objective of the course is twofold: one is to exercise a system
approach to enhance the teaching of the astronautic engineering.
The other is to organize a design team for the picosat project
in the universities. Some students from the class will be selected
to continue their involvement with the project. For those students
not going to continue their activities with the project, they
should be benefit from the course on system engineering concept
and basic knowledge of satellite design.
2. Course arrangement for the first semester of 2003:
The first semester including 18 weeks can be arranged as shown
in the attached course outline. Basically, we can categorize the
lecture material into "System" and "Subsystem"
and lecture level into "System Design" and "Conceptual/Preliminary
Design". The course in the first semester is devoted to the
"conceptual design" for both "system" and
"subsystem", while the second semester will emphasize
on the "preliminary design" of "subsystem".
The contents suggested for the 1st semester are:
Two
weeks are allocated for students to prepare their project report
for design review as midterm and final exam. To evaluate each
student's performance, we may rely on the inputs from team advisors
and team leaders, and the overall performance of the team.
3. Course material preparation:
A textbook is chosen, "Spacecraft Systems Engineering"
edited by P. Fortescue and J. Stark, for the class. The advantage
of using a textbook is that it would be easier for students to
follow and probably lecture material can be developed in a more
organized fashion. However, regardless what textbook we choose,
it most likely will not able to cover all the desired material
for the picosat design. Reading assignments of some reference
materials certainly can provide more information for students.
4. Conclusion:
The planning of the course is to provide students in the first
semester a basic idea of picosat design and the simulation technique
of how to evaluate some important design parameters. With more
detailed requirements in the second semester, the course will
emphasize on subsystem design and system integration. Obviously,
there are various ways to organize a course especially for the
unique subject of picosat design. A videoconference meeting may
be conducted to discuss further about textbook to be used or referenced,
arrangement of lecture subject, lecturer assignment, and guideline
for course material preparation.
參考書目:
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References Textbook:
W.
J. Larson and J. R. Wertz, (Editors), "Space Mission Analysis
and Design," Third Edition, ISBN: 0-881883-01-8, Microcosm,
Inc., Torrance, California, 1999.
Reference
books:
| 1. |
Brown,
C. D., "Spacecraft Mission Design," ISBN 1-56347-041-1,
AIAA Education Series, American Institute of Aeronautics
and Astronautics, Inc., Washington, DC, USA, 1992
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| 2. |
Griffin,
M. D., and French, J. R., "Space Vehicle Design,"
ISBN 0-930403-90-8, AIAA Education Series, American Institute
of Aeronautics and Astronautics, Inc., Washington, DC, USA,
1991
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| 3. |
Pisacane,
V. L. and Moore, R. C., (Editors), "Fundamentals of
Space Systems," ISBN: 0-19-507497-1, Oxford University
Press, New York, USA, 1994.
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| 4. |
Wertz,
J. R., (Editor): "Spacecraft Attitude Determination
and Control," D. Reidel, Dordrecht, Holland, 1978
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5.
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Hughes,
P. C., "Spacecraft Attitude Dynamics," ISBN 0-471-81842-9,
John Wiley & Sons, Inc., New York, 1986
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| 6. |
Hord,
R. M., "Remote Sensing: Methods and Applications,"
ISBN 0471-82824-6, John Wiley & Sons, Inc., New York,
1986
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| 7. |
Chetty,
P. R. K., "Satellite Technology and its Applications,"
ISBN 0-8306-2931-9, TAB Books, Inc., Blue Ridge Summit,
PA, 1988
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