摘要(英) |
Advanced Ionospheric Probe (AIP) is an all-in-one plasma sensor for the FORMOSAT-5 satellite to measure ionospheric plasma characteristics. Although a mounting space on the top panel is limited, a field of view (FOV) higher than 50° x 50° is required for the AIP to measure incoming ionic angles of arrival in most of orbital environment. Meanwhile, a mechanical design of the AIP shall meet all requirements of the FORMOSAT-5 satellite. In this report, the design of the AIP will be outlined and indicates that the FOV of the sensor can be achieved. The design is also verified by Dassault Systèmes SolidWorks Simulation 2011 in a static analysis, like mass, center of gravity, dimension, load factors, margin of safety, buckling safety margin, 1st mode natural frequency, and, in a dynamic analysis, like displacement, velocity, and acceleration of sine vibration. We carry out AIP thermal analysis with the satellite thermal model by use MSC/SINDA, give a range of the temperature. And the last one is the atomic oxygen analysis, which could sift material to follow the requirement. |
參考文獻 |
Adams V. and A. Askenazi, Building Better Products with Finite Element Analysis, OnWord Press, Santa Fe, NM, (1999).
Anderson, P. C. , Characteristics of spacecraft charging in low Earth orbit, J. Geophys. Res., 117, A07308, DOI:10.1029/2011JA016875 (2012).
Cremer L. and M. Heckl, Stucture-Borne Sound, Springer-Verlag, New York, (1988).
Davidson R. L. , G. D. Earle, J. H. Klenzing, and R. A. Heelis , A numerical study of geometry dependent errors in velocity, temperature, and density measurements from single grid planar retarding potential analyzers, (2010).
Dyne S.J.C., Tunbridge D.E.L., Collins P.P. , The vibration environment on a satellite in orbit, High Accuracy Platform Control in Space, IEEE Colloquium on, 12/1-12/6, (1993).
Edward M. Silverman, Space Environmental Effects on Spacecraft: LEO Materials Selection Guide, NASA CR-4661, (1995).
FORMOSAT-5 Spacecraft Bus to Science Payload Interface Requirement Document, FS5-IRD-0001, (2011).
FORMOSAT-5 AIP Mechanical Structure Analysis Report, FS5SPL-MECH-ANLYS, (2012).
FORMOSAT-5 AIP Thermal Analysis Report, FS5SPL-THER-ANLYS, (2012).
FORMOSAT-5 AIP Atomic Oxygen Analysis Report, FS5SPL-AO-ANLYS. (2013).
Huddlestone, R. H. and Leonard, S. L., Plasma Diagnostic Techniques, (1968).
Juvinall, R: Stress, Strain, and Strength, section 14.13, Page 295. McGraw-Hill, (1967).
McCormick, Barnes W., Aerodynamics, Aeronautics and Flight Mechanics. John Wiley & Sons. New York ISBN 0-471-03032-5 (1979).
NASA Contractor Report 4661 Part 1, Space Environmental Effect on Spacecraft: LEO Material Selection Guide, (1995).
NASA-STD-5001, Structural Design and Test Factors for Spaceflight Hardware, section 3. NASA, (2008).
NASA/TP-1999-209260, Material Selection Guidelines to Limit Atomic Oxygen Effects on Spacecraft Surfaces, (1999).
胡紹賢,太空電漿探針系統,碩士論文,2007.
林再文,太空離子探測系統,碩士論文,2010.
朱宴達,微衛星離子探測系統,碩士論文,2011.
實威國際,SolidWorks Simulation原廠教育訓練手冊,易習圖書,2011. |