Ku Band Waveguide Diplexer Design for Satellite Communication Implementation by Additive Manufacturing and Experimental Characterization

Total Page:16

File Type:pdf, Size:1020Kb

Ku Band Waveguide Diplexer Design for Satellite Communication Implementation by Additive Manufacturing and Experimental Characterization Universidad Politécnica de Madrid Escuela Técnica Superior de Ingenieros de Telecomunicación TRABAJO FIN DE GRADO Ku band waveguide diplexer design for satellite communication Implementation by additive manufacturing and experimental characterization MADRID, 2015 IRENE ORTIZ DE SARACHO PANTOJA Trabajo Fin de Grado Ku band waveguide diplexer design for satellite communica- tion. Implementation by additive manufacturing and experi- mental characterization Autor Irene Ortiz de Saracho Pantoja Tutor José Ramón Montejo Garai Departamento Señales, Sistemas y Radiocomunicaciones Tribunal Presidente: D. Juan Enrique Page de la Vega Vocal: D. Javier Gismero Menoyo Secretario: D. José Ramón Montejo Garai Suplente: D. Mariano Barba Gea Fecha de lectura: Calificación: Universidad Politécnica de Madrid Escuela Técnica Superior de Ingenieros de Telecomunicación TRABAJO FIN DE GRADO Ku band waveguide diplexer design for satellite communication Implementation by additive manufacturing and experimental characterization MADRID, 2015 IRENE ORTIZ DE SARACHO PANTOJA Abstract A great amount of telecommunication services such as television distribution or navigation systems are based on satellite communication. As it occurs in other spatial applications, there are some key resources which are severely limited on board spacecrafts, as mass or volume. In this sense, one of the most important passive devices, which allows a better use of such resources, is the diplexer of the feed antenna system. This device enables the use of one single antenna for both transmission and reception channels, resulting in an optimization of the above resources. The main goal of this work is to design a diplexer fulfilling real satellite-communication specifications. This device consists in two filtering structures joined by a three-port junction. In addition, the use of waveguide technology is imperative, due to the high power level handled. The diplexer design is accomplished by dividing the structure in separate parts, in order to make the process feasible and efficient. Firstly, different filter configurations are developed – high-, low- and band- pass responses –, even though only two of them will be diplexed. When tackling their initial design, a theoretic synthesis is performed through the use of circuit models. The filters are subsequently optimized by using full-wave CAD techniques, particularly mode matching. At this point it is essential to analyze the structures and their symmetry in order to determine which modes are actually propagating, to reduce computational effort. Finally, FEM method is used to verify the results previously obtained. Once the filter design is concluded, the three-port-junction dimensions are calculated. Eventually, the whole diplexer is optimized to fit the electric specifications. Furthermore, this work presents a brand-new added value: the physical implementation and experimental characterization of both the diplexer and the filters. This possibility, unfeasible until now because of its high cost, derives from the development of additive manufacturing techniques. The prototypes are printed in plastic (PLA) by means of a low-cost 3D-printer, and afterwards metallized. This technology entails two different limitations: the precision of the geometric dimensions (±0.2 mm) and the conductivity of the metallic paint which covers the walls of the waveguide. A comparison between simulated and measured values is included in this work, as well as an analysis of the experimental results. In summary, this work expounds a real engineering process: the problem of designing a device which satisfies real specifications, the limitations caused by a manufacturing process, the eventual experimental characterization and the inference of conclusions. Keywords: diplexer, waveguide filter, Ku band, satellite communication, additive manufacturing Resumen Gran cantidad de servicios de telecomunicación tales como la distribución de televisión o los sistemas de navegación están basados en comunicaciones por satélite. Del mismo modo que ocurre en otras aplicaciones espaciales, existe una serie de recursos clave severamente limitados, tales como la masa o el volumen. En este sentido, uno de los dispositivos pasivos más importantes es el diplexor del sistema de alimentación de la antena. Este dispositivo permite el uso de una única antena tanto para transmitir como para recibir, con la consiguiente optimización de recursos que eso supone. El objetivo principal de este trabajo es diseñar un diplexor que cumpla especificaciones reales de comu- nicaciones por satélite. El dispositivo consiste en dos estructuras filtrantes unidas por una bifurcación de tres puertas. Además, es imprescindible utilizar tecnología de guía de onda para su implementación debido a los altos niveles de potencia manejados. El diseño del diplexor se lleva a cabo dividiendo la estructura en diversas partes, con el objetivo de que todo el proceso sea factible y eficiente. En primer lugar, se han desarrollado filtros con diferentes respuestas – paso alto, paso bajo y paso banda – aunque únicamente dos de ellos formarán el diplexor. Al afrontar su diseño inicial, se lleva a cabo un proceso de síntesis teórica utilizando modelos circuitales. A continuación, los filtros se optimizan con técnicas de diseño asistido por ordenador (CAD) full-wave, en concreto mode matching. En este punto es esencial analizar las estructuras y su simetría para determinar qué modos electromagnéticos se están propagando realmente por los dispositivos, para así reducir el esfuerzo computacional asociado. Por último, se utiliza el Método de los Elementos Finitos (FEM) para verificar los resultados previamente obtenidos. Una vez que el diseño de los filtros está terminado, se calculan las dimensiones correspondientes a la bifurcación. Finalmente, el diplexor al completo se somete a un proceso de optimización para cumplir las especificaciones eléctricas requeridas. Además, este trabajo presenta un novedoso valor añadido: la implementación física y la caracterización experimental tanto del diplexor como de los filtros por separado. Esta posibilidad, impracticable hasta ahora debido a su elevado coste, se deriva del desarrollo de las técnicas de manufacturación aditiva. Los prototipos se imprimen en plástico (PLA) utilizando una impresora 3D de bajo coste y posteriormente se metalizan. El uso de esta tecnología conlleva dos limitaciones: la precisión de las dimensiones geométricas (±0.2 mm) y la conductividad de la pintura metálica que recubre las paredes internas de las guías de onda. En este trabajo se incluye una comparación entre los valores medidos y simulados, así como un análisis de los resultados experimentales. En resumen, este trabajo presenta un proceso real de ingeniería: el problema de diseñar un dispositivo que satisfaga especificaciones reales, las limitaciones causadas por el proceso de fabricación, la posterior caracterización experimental y la obtención de conclusiones. Palabras clave: diplexor, filtro en guía de onda, banda Ku, comunicaciones por satélite, manufac- turación aditiva Para M., por cuidar de mis neuronas. Para J.R., por intentar que salieran cestos con los mimbres que había. Contents 1 Introduction and design specifications 2 2 Waveguides as transmission lines 4 2.1 Propagation in rectangular waveguides . .4 2.2 Attenuation in rectangular waveguides . .6 2.3 Waveguide implementation of filtering structures . .7 2.3.1 Low-pass filters . .7 2.3.2 High-pass filters . .8 2.3.3 Band-pass filters . .9 3 Modal analysis as full-wave design technique 10 3.1 Symmetry and its implications . 11 4 Low-pass filter 13 5 High-pass filter 15 6 Band-pass filters 17 6.1 Synthesis process . 18 6.1.1 Chebychev filters and low-pass response . 18 6.1.2 J-inverters and band-pass transformation . 19 6.1.3 Slope parameter and distributed resonators . 21 6.2 Physical dimensions . 22 6.3 Optimization and final response . 24 6.3.1 TX filter . 24 6.3.2 RX filter . 25 7 Diplexer 26 7.1 Main challenges when designing a diplexer . 27 7.2 Junction design and final optimization . 29 7.3 Double bend . 32 7.4 Diplexer . 34 8 Manufacture and losses 35 8.1 Additive Manufacturing (AM) . 35 8.2 Low-cost 3D printing and RepRap . 36 8.3 Challenges and limitations of 3D printing . 36 8.4 Metallization process . 38 8.5 Conduction losses . 39 9 Measurement and analysis of results 41 9.1 Low-pass filter . 42 9.2 High-pass filter . 43 9.3 Band-pass reception filter . 45 9.4 Diplexer . 47 10 Conclusions 48 11 Future work 50 12 Contributions 50 References 51 1 1 Introduction and design specifications Satellite communication is one of the most important space applications. It encompasses many services used by millions of people every day, such as television broadcast or navigation systems. It also includes less-known services, for instance tele-medicine. Besides, the importance of mobile satellite systems to connect remote areas with the rest of the world must not be forgotten. This variety of applications makes satellite communication a very mature and developed field, with certain peculiarities. Design specifications of the passive microwave devices on board spacecrafts are practically unique, since there is a great amount of satellites, each of them working in different orbits and frequencies. Satellite frequencies range from 3 to 30 GHz (Super High Frequency). However, this wide spectrum is divided into sub bands, each of them devoted to certain applications. Power levels handled also depend on the different purposes. Besides, the architecture of each satellite launched into orbit presents
Recommended publications
  • Tr-Sas-076-All
    NORTH ATLANTIC TREATY RESEARCH AND TECHNOLOGY ORGANISATION ORGANISATION AC/323(SAS-076)TP/430 www.rto.nato.int RTO TECHNICAL REPORT TR-SAS-076 NATO Independent Cost Estimating and the Role of Life Cycle Cost Analysis in Managing the Defence Enterprise (Estimation indépendante des coûts de l’OTAN et rôle de l’analyse des coûts globaux de possession au sein de l’OTAN) This Report presents the findings of Task Group SAS-076. Published August 2012 Distribution and Availability on Back Cover NORTH ATLANTIC TREATY RESEARCH AND TECHNOLOGY ORGANISATION ORGANISATION AC/323(SAS-076)TP/430 www.rto.nato.int RTO TECHNICAL REPORT TR-SAS-076 NATO Independent Cost Estimating and the Role of Life Cycle Cost Analysis in Managing the Defence Enterprise (Estimation indépendante des coûts de l’OTAN et rôle de l’analyse des coûts globaux de possession au sein de l’OTAN) This Report presents the findings of Task Group SAS-076. The Research and Technology Organisation (RTO) of NATO RTO is the single focus in NATO for Defence Research and Technology activities. Its mission is to conduct and promote co-operative research and information exchange. The objective is to support the development and effective use of national defence research and technology and to meet the military needs of the Alliance, to maintain a technological lead, and to provide advice to NATO and national decision makers. The RTO performs its mission with the support of an extensive network of national experts. It also ensures effective co-ordination with other NATO bodies involved in R&T activities. RTO reports both to the Military Committee of NATO and to the Conference of National Armament Directors.
    [Show full text]
  • Optical – Near-Infrared Catalog for the AKARI North Ecliptic Pole Deep field
    A&A 566, A60 (2014) Astronomy DOI: 10.1051/0004-6361/201322561 & c ESO 2014 Astrophysics Optical – near-infrared catalog for the AKARI north ecliptic pole Deep field Nagisa Oi1, Hideo Matsuhara1, Kazumi Murata1,2, Tomotsugu Goto3, Takehiko Wada1, Toshinobu Takagi1, Youichi Ohyama4, Matthew Malkan5, Myungshin Im6, Hyunjin Shim6,7, Stephen Serjeant8, and Chris Pearson8,9,10 1 Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Sagamihara, 252-5210 Kanagawa, Japan e-mail: [email protected] 2 Department of Space and Astronautical Science, The Graduate University for Advanced Studies, 753-8511 Yamaguchi, Japan 3 Institute of Astronomy and Department of Physics, National Tsing Hua University No. 101, Section 2, Kuang-Fu Road, Hsinchu 30013, Taiwan, R.O.C. 4 Academia Sinica, Institute of Astronomy and Astrophysics, 11F of Astronomy-Mathematics Building, National Taiwan University, No.1, Sec. 4, Roosevelt Rd, 10617 Taipei, Taiwan R.O.C. 5 Department of Physics and Astronomy, UCLA, Los Angeles, CA 90095-1547, USA 6 Department of Physics & Astronomy, FPRD, Seoul National University, Shillim-Dong, Kwanak-Gu, 151-742 Seoul, Korea 7 Department of Earth Science Education, Kyungpook National University, 702-701 Daegu, Republic of Korea 8 Astrophysics Group, Department of Physics, The Open University, Milton Keynes, MK7 6AA, UK 9 RAL Space, Rutherford Appleton Laboratory, Harwell Oxford, OX11 0QZ, UK 10 Oxford Astrophysics, Oxford University, Keble Road, Oxford OX1 3RH, UK Received 29 August 2013 / Accepted 18 March 2014 ABSTRACT ∗ Aims. We present an 8-band (u , g , r , i , z , Y, J, Ks) optical to near-infrared deep photometric catalog based on the observations made with MegaCam and WIRCam at the CFHT, and compute photometric redshifts, zp in the north ecliptic pole (NEP) region.
    [Show full text]
  • For Each Service They Propose at the Time They File Their Applications, and to Preempt State Regulation to the Maximum Extent Possible
    for each service they propose at the time they file their applications, and to preempt state regulation to the maximum extent possible. III. CONCLUSION Viacom submits that the assignment of fixed frequency pairs to PCS licensees will result in higher relocation costs and lengthy delays in the provision of PCS service. Accordingly, Viacom recommends that the FCC adopt the Spectral Zone Coordination approach, under which two PCS licensees in a market are each assured a fixed allocation of 25 MHz in the 1850-1990 MHz band. Under this approach, in the event there is blockage within any PCS licensee's fixed allocation, each PCS licensee would have the flexibility to select needed frequencies within any unused portion of the 1850-1990 MHz band (such unused portion totalling 70 MHz if the FCC allocates 20 MHz to unlicensed services) for any given cell site pending completion of voluntary negotiations or ultimately arbitration and involuntary relocation, thereby minimizing the need for the relocation of incumbents and producing a variety of options for the few required relocations. Alternatively, if the FCC decides, as it has proposed, to allocate three frequency blocks of 30 MHz each, Viacom recommends that the FCC apply the Spectral Zone Coordination technique to its proposed fixed block scheme, providing for a 30 MHz pool which can be accessed by PCS operators on a notification basis until incumbent users relocate as necessary. This type of - 22 - approach will retain most of the advantages of a fixed block scheme while adding much of the flexibility of the Spectral Zone Coordination methodology.
    [Show full text]
  • Design and Development of a Ka-Band Interferometer for Cryospheric Applications Harish K
    University of Massachusetts Amherst ScholarWorks@UMass Amherst Masters Theses 1911 - February 2014 2009 Design and Development of a Ka-band Interferometer for Cryospheric Applications Harish K. Vedantham University of Massachusetts Amherst Follow this and additional works at: https://scholarworks.umass.edu/theses Part of the Electrical and Electronics Commons, and the Electromagnetics and Photonics Commons Vedantham, Harish K., "Design and Development of a Ka-band Interferometer for Cryospheric Applications" (2009). Masters Theses 1911 - February 2014. 220. Retrieved from https://scholarworks.umass.edu/theses/220 This thesis is brought to you for free and open access by ScholarWorks@UMass Amherst. It has been accepted for inclusion in Masters Theses 1911 - February 2014 by an authorized administrator of ScholarWorks@UMass Amherst. For more information, please contact [email protected]. DESIGN AND DEVELOPMENT OF A KA-BAND INTERFEROMETER FOR CRYOSPHERIC APPLICATIONS A Thesis Presented by HARISH VEDANTHAM Submitted to the Graduate School of the University of Massachusetts Amherst in partial fulfillment of the requirements for the degree of MASTER OF SCIENCE IN ELECTRICAL AND COMPUTER ENGINEERING February 2009 Electrical and Computer Engineering DESIGN AND DEVELOPMENT OF A KA-BAND INTERFEROMETER FOR CRYOSPHERIC APPLICATIONS A Thesis Presented by HARISH VEDANTHAM Approved as to style and content by: Paul R. Siqueira, Chair Stephen J. Frasier, Member Daniel H. Schaubert, Member Christopher V. Hollot, Department Chair Electrical and Computer Engineering For my mother, father and sister This Earth is His, to Him belong those vast and boundless skies, Both seas within Him rest, and yet in that small pool He lies. Atharva Veda 12th century BC iv ACKNOWLEDGMENTS I have had an enjoyable and rewarding time working at the Microwave Remote Sensing Lab.
    [Show full text]
  • (12) United States Patent (10) Patent No.: US 8,019,275 B2 Norin Et Al
    USO080 19275 B2 (12) United States Patent (10) Patent No.: US 8,019,275 B2 Norin et al. (45) Date of Patent: *Sep. 13, 2011 (54) BAND UPCONVERTER APPROACH TO (52) U.S. Cl. ....................... 455/3.02:455/12.1; 455/427 KAAKU SIGNAL DISTRIBUTION (58) Field of Classification Search ........ 455/3.01-3.06, 455/427 430, 12.1-13.3, 168.1, 176.1, 190.1, (75) Inventors: John Norin, Redondo Beach, CA (US); 455/313, 334; 370/316 Kesse Ho, Westminster, CA (US) See application file for complete search history. (56) References Cited (73) Assignee: The DIRECTV Group, Inc., El Segundo, CA (US) U.S. PATENT DOCUMENTS 3,581,209 A 5, 1971 Zimmerman *) Notice: Subject to anyy disclaimer, the term of this 3,670,275 A 6, 1972 Kalliomaki et al. patent is extended or adjusted under 35 4,064,460 A 12/1977 Gargini 4,132,952 A 1/1979 Honguet al. U.S.C. 154(b) by 947 days. 4,354,167 A 10, 1982 Terreault et al. This patent is Subject to a terminal dis 4,382.266 A 5, 1983 Panzer claimer. 4,397,037 A 8, 1983 Theriault 4,403,343 A 9, 1983 Hamada 4,509, 198 A 4, 1985 Nagatomi (21) Appl. No.: 11/546,117 4.513,315 A 4, 1985 Dekker et al. (22) Filed: Oct. 11, 2006 (Continued) FOREIGN PATENT DOCUMENTS (65) Prior Publication Data CN 1413021 4/2003 US 2007/OO83898A1 Apr. 12, 2007 (Continued) Related U.S. Application Data OTHER PUBLICATIONS (60) Provisional application No.
    [Show full text]
  • Absorption, Fluorescence and Emission Anisotropy Spectra of 4-Cyano-N,N-Dimethylaniline in Different Media and at Different Temperatures
    Absorption, Fluorescence and Emission Anisotropy Spectra of 4-Cyano-N,N-dimethylaniline in Different Media and at Different Temperatures A. Kawski and G. Piszczek Luminescence Research Group, Institute of Experimental Physics, University of Gdansk, ul. Wita Stwosza 57, 80-952 Gdansk, Poland Z. Naturforsch. 52a, 409-414 (1997); received March 3, 1997 The effect of temperature on fluorescence and emission anisotropy spectra of 4-cyano-N,N- dimethylaniline (CDMA) was investigated in viscous (glycerol and paraffin oil) and rigid (polyvinyl alcohol) PVA and polyvinyl chloride) PVC) media. A strong effect of temperature on the intensity of a and b emission bands was observed. It was also found that the emission anisotropy, r, does not vary in the longwave emission band a at a fixed temperature but decreases in the emission band b together with the decreasing wavelength. The latter effect is due to the fact that the transition moment in this band is perpendicular to the long axis of the CDMA molecule. For CDMA in paraffin oil, a normal b band with negative emission anisotropy only occurs. In all other media used, the emission anisotropy has lower values, approaching zero, which results from the considerable covering of band b with a broad emission band a. 1. Introduction It was demonstrated in addition that the original 1 1 hypothesis [1, 5, 8] of solvated-induced Lb/ La state The investigations of Lippert et al. [1-4] concern- crossing may be combined with the twisted internal ing light polarization (emission anisotropy) in the ab- charge transfer (TICT) mechanism [9,10] to form a sorption and fluorescence bands of p-cyano-N,N- consistent intramolecular reaction model [3, 11].
    [Show full text]
  • The Origin of UV / Optical Variability of AGN: Relationship to X-Ray Variability
    The origin of UV / Optical Variability of AGN: Relationship to X-ray Variability Ian McHardy University of Southampton 1 Southampton Main Questions • What drives UV/optical variability in AGN? • How is the X-ray band related to UV/optical? • What do X-ray/UV/optical variations tell us about AGN inner structure? 2 Southampton Possible drivers of UV/optical Variability - Reprocessing of higher energy photons - which “high” energy? X-ray? Far-UV? - reprocessing off what? Disc? BLR? - Intrinsic disc variations 3 Southampton Observational Diagnostics • Reprocessing - High energies lead uv/optical by short (hour-days) light travel time. Allows ‘reverberation’ mapping of reprocessing structures. Measure lag from different temperature regions (different λ ). • Intrinsic disc variability – High energies lag: two possibilities – Long lag (months), viscous propagation timescale for perturbations to reach X-ray region from optical in disc – Short lag (hour-day), light travel time of UV seed photons to corona 4 REPROCESSING Southampton Wavelength dependence of lags For standard Shakura-Sunyaev DISC, 4 −1 −3 L(R)=σT ∝MBH . m! E R dissipating gravitational potential energy ! ( R in gravitational radii) −1/4 1/4 −3/4 i.e. T ∝ M m! R BH E Disc illumination from point source, height H above disc, also falls off as H R-3 So for reprocessing 4/3 Lag ∝Wavelength (eg Cackett et al 2007) from disc, we expect and Lag ∝M2/3m! 1/3 ! E For illumination of a shell-type structure, eg the BLR or torus, Illumination falls of as R-2 giving Lag ∝Wavelength2 5 Southampton
    [Show full text]
  • Polarimetric Remote Sensing in Oxygen a and B Bands: Sensitivity Study and Information Content Analysis for Vertical Profile of Aerosols
    Atmos. Meas. Tech., 9, 2077–2092, 2016 www.atmos-meas-tech.net/9/2077/2016/ doi:10.5194/amt-9-2077-2016 © Author(s) 2016. CC Attribution 3.0 License. Polarimetric remote sensing in oxygen A and B bands: sensitivity study and information content analysis for vertical profile of aerosols Shouguo Ding1,a, Jun Wang1, and Xiaoguang Xu1 1Department of Earth and Atmospheric Sciences, University of Nebraska Lincoln, Lincoln, NE 68588, USA anow at: Earth Resources Technological Inc., Laurel, MD 20707, USA Correspondence to: Jun Wang ([email protected]) Received: 5 November 2015 – Published in Atmos. Meas. Tech. Discuss.: 18 January 2016 Revised: 18 April 2016 – Accepted: 25 April 2016 – Published: 11 May 2016 Abstract. Theoretical analysis is conducted to reveal the in- spheric window channels for retrieving the vertical profiles formation content of aerosol vertical profile in space-borne of aerosols, especially highly scattering aerosols, over land. measurements of the backscattered radiance and degree of linear polarization (DOLP) in oxygen (O2/ A and B bands. Assuming a quasi-Gaussian shape for aerosol vertical pro- file characterized by peak height H and half width γ (at half 1 Introduction maximum), the Unified Linearized Vector Radiative Trans- fer Model (UNL-VRTM) is used to simulate the Stokes four- Aerosols are ubiquitous in the atmosphere and play an im- vector elements of upwelling radiation at the top of atmo- portant role in the climate system through their direct effects sphere (TOA) and their Jacobians with respect to H and γ . on the transfer of radiative energy (Forster et al., 2007) and Calculations for different aerosol types and different combi- indirect effects on cloud microphysical properties by serving nations of H and γ values show that the wide range of gas as cloud condensation nuclei (Twomey, 1977).
    [Show full text]
  • Standard Photometric Systems
    7 Aug 2005 11:27 AR AR251-AA43-08.tex XMLPublishSM(2004/02/24) P1: KUV 10.1146/annurev.astro.41.082801.100251 Annu. Rev. Astron. Astrophys. 2005. 43:293–336 doi: 10.1146/annurev.astro.41.082801.100251 Copyright c 2005 by Annual Reviews. All rights reserved STANDARD PHOTOMETRIC SYSTEMS Michael S. Bessell Research School of Astronomy and Astrophysics, The Australian National University, Weston, ACT 2611, Australia; email: [email protected] KeyWords methods: data analysis, techniques: photometric, spectroscopic, catalogs ■ Abstract Standard star photometry dominated the latter half of the twentieth century reaching its zenith in the 1980s. It was introduced to take advantage of the high sensitivity and large dynamic range of photomultiplier tubes compared to photographic plates. As the quantum efficiency of photodetectors improved and the wavelength range extended further to the red, standard systems were modified and refined, and deviations from the original systems proliferated. The revolutionary shift to area detectors for all optical and IR observations forced further changes to standard systems, and the precision and accuracy of much broad- and intermediate-band photometry suffered until more suitable observational techniques and standard reduction procedures were adopted. But the biggest revolution occurred with the production of all-sky photometric surveys. Hipparcos/Tycho was space based, but most, like 2MASS, were ground-based, dedicated survey telescopes. It is very likely that in the future, rather than making a measurement of an object in some standard photometric system, one will simply look up the magnitudes and colors of most objects in catalogs accessed from the Virtual Observatory.
    [Show full text]
  • University of Oklahoma Graduate College
    UNIVERSITY OF OKLAHOMA GRADUATE COLLEGE FREQUENCY-AGILE MICROWAVE FILTERS FOR RADARS WITH SIMULTANEOUS TRANSMISSION AND RECEPTION A DISSERTATION SUBMITTED TO THE GRADUATE FACULTY in partial fulfillment of the requirements for the Degree of DOCTOR OF PHILOSOPHY By SHAHROKH SAEEDI Norman, Oklahoma 2015 FREQUENCY-AGILE MICROWAVE FILTERS FOR RADARS WITH SIMULTANEOUS TRANSMISSION AND RECEPTION A DISSERTATION APPROVED FOR THE SCHOOL OF ELECTRICAL AND COMPUTER ENGINEERING BY Dr. Hjalti H. Sigmarsson, Chair Dr. Yang Hong Dr. Mark Yeary Dr. Jessica Ruyle Dr. Caleb J. Fulton c Copyright by SHAHROKH SAEEDI 2015 All Rights Reserved. This dissertation is dedicated to my dear wife. None of this would have been possible without her unconditional love and support. iv Acknowledgments The completion of this work would not have been possible without the help and encouragement of many people. First, I would like to sincerely thank my research advisor Professor Hjalti Sigmarsson for his continuous support, patient mentoring, supportive advising and encouragement. I am particularly grateful to him for the opportunity he provided for me to conduct independent research. Professor Sigmarsson has provided invaluable vision and a wealth of technical guidance throughout my graduate studies at the University of Ok- lahoma. I have deeply admired his commitment to academic excellence and dedication to the community and the society. I also sincerely thank my other committee members, Professor Mark Yeary, Professor Yang Hong, Professor Jessica Ruyle, and Professor Caleb Fulton for their interest and valuable ex- pertise, time, and effort in advising my dissertation work. I also wish to thank Professor Juseop Lee for his support, discussions and guidance throughout my research.
    [Show full text]
  • Zodiacal Light Beyond Earth Orbit Observed with Pioneer 10
    The Astronomical Journal, 156:86 (6pp), 2018 September https://doi.org/10.3847/1538-3881/aad0f0 © 2018. The American Astronomical Society. All rights reserved. Zodiacal Light Beyond Earth Orbit Observed with Pioneer 10 T. Matsumoto1,4 , K. Tsumura2 , Y. Matsuoka3, and J. Pyo4 1 Department of Space Astronomy and Astrophysics, Institute of Space and Astronoutical Science, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa 252- 5210, Japan 2 Frontier Research Institute for Interdisciplinary Science, Tohoku University, Sendai, Miyagi 980-8578, Japan 3 Research Center for Space and Cosmic Evolution, Ehime University, Matsuyama, Ehime 790-8577, Japan 4 Korea Astronomy and Space Science Institute (KASI), Daejeon 34055, Korea Received 2017 November 27; revised 2018 June 25; accepted 2018 June 28; published 2018 August 9 Abstract We reanalyze the Imaging Photopolarimeter data from Pioneer 10 to study the zodiacal light in the B and R bands beyond Earth orbit, applying an improved method to subtract integrated star light (ISL) and diffuse Galactic light (DGL). We found that there exists a significant instrumental offset, making it difficult to examine the absolute sky brightness. Instead, we analyzed the differential brightness, i.e., the difference in sky brightness from the average at high ecliptic latitude, and compared with that expected from the model zodiacal light. At a heliocentric distance of r<2 au, we found a fairly good correlation between the J-band model zodiacal light and the residual sky brightness after subtracting the ISL and DGL. The reflectances of the interplanetary dust derived from the correlation study are marginally consistent with previous works. The zodiacal light is not significantly detectable at r>3 au, as previously reported.
    [Show full text]
  • Radio Frequency and Modulation Systems—Part 1: Earth Stations
    CCSDS Historical Document This document’s Historical status indicates that it is no longer current. It has either been replaced by a newer issue or withdrawn because it was deemed obsolete. Current CCSDS publications are maintained at the following location: http://public.ccsds.org/publications/ CCSDS HISTORICAL DOCUMENT Recommendations for Space Data System Standards RADIO FREQUENCY AND MODULATION SYSTEMS— PART 1 EARTH STATIONS AND SPACECRAFT RECOMMENDED STANDARD CCSDS 401.0-B BLUE BOOK October 2014 CCSDS HISTORICAL DOCUMENT Recommendations for Space Data System Standards RADIO FREQUENCY AND MODULATION SYSTEMS— PART 1 EARTH STATIONS AND SPACECRAFT RECOMMENDED STANDARD CCSDS 401.0-B BLUE BOOK October 2014 CCSDS HISTORICAL DOCUMENT CCSDS RECOMMENDATIONS FOR RADIO FREQUENCY AND MODULATION SYSTEMS Earth Stations and Spacecraft AUTHORITY Issue: Recommended Standard, Issue 24 Date: October 2014 Location: Washington, DC, USA This document has been approved for publication by the Management Council of the Consultative Committee for Space Data Systems (CCSDS) and represents the consensus technical agreement of the participating CCSDS Member Agencies. The procedure for review and authorization of CCSDS documents is detailed in Organization and Processes for the Consultative Committee for Space Data Systems (CCSDS A02.1-Y-4), and the record of Agency participation in the authorization of this document can be obtained from the CCSDS Secretariat at the e-mail address below. This document is published and maintained by: CCSDS Secretariat National Aeronautics and Space Administration Washington, DC, USA E-mail: [email protected] CCSDS 401 B Page i October 2014 CCSDS HISTORICAL DOCUMENT CCSDS RECOMMENDATIONS FOR RADIO FREQUENCY AND MODULATION SYSTEMS Earth Stations and Spacecraft STATEMENT OF INTENT The Consultative Committee for Space Data Systems (CCSDS) is an organization officially established by the management of its members.
    [Show full text]