Ultra-Wideband WDM Optical Network Optimization
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Overview of Sensors for Applications
OVERVIEW OF SENSORS FOR APPLICATIONS Deepak Putrevu Head, MTDD/AMHTDG EM SPECTRUM Visible 0.4-0.7μm Near infrared (NIR) 0.7-1.5μm Optical Infrared Shortwave infrared (SWIR) 1.5-3.0μm Mid-wave infrared (MWIR) 3.0-8.0μm (OIR) Region Longwave IR(LWIR)/Thermal IR(TIR) 8.0-15μm Far infrared (FIR) Beyond15μm Gamma Rays X Rays UV Visible NIR SWIR Thermal IR Microwave P-band: ~0.25 – 1 GHz Microwave Region L-band: 1 -2 GHz S-band: 2-4 GHz •Sensors are 24x365 C-band: 4-8 GHz •Signal data characteristics X-band: 8-12 GHz unique to the microwave region of the EM spectrum Ku-band: 12-18 GHz K-band: 18-26 GHz •Response is primarily governed by geometric Ka-band: 26-40 GHz structures and hence V-band: 40 - 75 GHz complementary to optical W-band: 75-110 GHz imaging mm-wave: 110 – 300GHz Basic Interactions between Electromagnetic Energy and the Earth’s Surface Incident Power reflected, ρP Reflectivity: The fractional part of the radiation, P incident radiation that is reflected by the surface. Power absorbed, αP Absorptivity: the fractional part of the = Power emitted, εP incident radiation that is absorbed by the surface. Power transmitted, τP Emissivity: The ratio of the observed flux emitted by a body or surface to that of a P= Pr + Pt + Pa blackbody under the same condition. 푃 푃 푃 푟 + 푡 + 푎 = 1 푃 푃 푃 Transmissivity: The fractional part of the ρ + τ + α =1 radiation transmitted through the medium. At thermal equilibrium, absorption and emission are the same. -
Advances in Satellite Technologies- ISRO Initiatives
Advances in Satellite Technologies- ISRO Initiatives Sumitesh Sarkar Space Applications Centre (ISRO) March 27, 2019 National Workshop on Advances in Satellite Technologies National Workshop on Advances in Satellite Technologies - Mach 27, 2019 Advance Technology : Key Areas Migration from Broadcast/VSAT centric to Data-centric Payload design - HTS . Multi-beam coverage in Ku and Ka-band ensuring Frequency Reuse and enhanced Payload performance . Increased Payload Hardware – need for miniaturization . Addressing new applications like Mobile backhauling, In-Flight Connectivity etc. Special focus on unserved/underserved regions within India Use of Higher frequency bands – Ku to Ka to Q/V band . Migration to higher frequency bands – ‘User ‘ as well as ‘Feeder’ links . More interference free Spectrum . Constraints of available technologies Redefining MSS with enhanced capabilities . Multi-beam High power transponders in S-band - enabling SDMB services National Workshop on Advances in Satellite Technologies - Mach 27, 2019 2 Evolution in On-board Antenna Technology Single Circular beam Shaped Beam Multibeam(HTS) (Dual Gridded Reflector) National Workshop on Advances in Satellite Technologies - Mach 27, 2019 Technology Trends – Active Low power RF Circuits MMIC SOC 9mm X 6mm Ka-band (In test) 100mmx40mm 70mmx60mm x25mm x22mm based based MMIC die in pac. pac. MMIC Chip MMIC LTCC pac. Qualified (In BB test) 100mmx100mm x25mm Gen In production by industry nd MIC based MIC 2 RF Technologies RF 170mmx100mmx35mm MIC MIC based 200mmx180mmx100mm (2RF sec.) 1stgen. INSAT-2A to INSAT-2D INSAT-3 and 4 Series GSAT-5 GSAT-7/11 Future technologies Payload Generation National Workshop on Advances in Satellite Technologies - Mach 27, 2019 High Throughput Satellite : GSAT-11 Features: . -
Spectrum and the Technological Transformation of the Satellite Industry Prepared by Strand Consulting on Behalf of the Satellite Industry Association1
Spectrum & the Technological Transformation of the Satellite Industry Spectrum and the Technological Transformation of the Satellite Industry Prepared by Strand Consulting on behalf of the Satellite Industry Association1 1 AT&T, a member of SIA, does not necessarily endorse all conclusions of this study. Page 1 of 75 Spectrum & the Technological Transformation of the Satellite Industry 1. Table of Contents 1. Table of Contents ................................................................................................ 1 2. Executive Summary ............................................................................................. 4 2.1. What the satellite industry does for the U.S. today ............................................... 4 2.2. What the satellite industry offers going forward ................................................... 4 2.3. Innovation in the satellite industry ........................................................................ 5 3. Introduction ......................................................................................................... 7 3.1. Overview .................................................................................................................. 7 3.2. Spectrum Basics ...................................................................................................... 8 3.3. Satellite Industry Segments .................................................................................... 9 3.3.1. Satellite Communications .............................................................................. -
L-Shaped Monopole Antenna with Modified Partial Ground Plane for Multiband Operation
International Journal of Innovative Technology and Exploring Engineering (IJITEE) ISSN: 2278-3075, Volume-8 Issue-10, August 2019 L-Shaped Monopole Antenna with Modified Partial Ground Plane for Multiband Operation Prachi Pandey, Neelesh Agrawal, Mukesh Kumar, Navendu Nitin, Anil Kumar Abstract- In this paper a design of L-shaped monopole In [4] a meandered T-shaped monopole is proposed for antenna (LMA) with modified partial ground plane for multiband 2.45/5.2/5.8 GHz LAN operations with a long and a short operation is presented. The `dimension of proposed antenna is arm strip extended from the feedline. A compact improved 40× 47 mm2 with 1.6 height using Teflon substrate having T-Form monopole antenna [5] using two asymmetric dielectric constant 2.1. The ground plane is amended by inserting horizontal strips has been designed to achieve multiband an anti-symmetric horizontal L-slots. Single band to multiband behaviour is accomplished by applying two horizontal L-slots on operation. In [6] a C-shaped monopole antenna is designed partial ground plane of LMA. Both the slots are antisymmetric to having a shorted parasitic strip to obtain two separate Y-axis. The parametric study has also been done which is impedance bandwidth. Frequency agility, improved gain and responsible for antenna behaviour. The operating frequency beam forming can be attained by applying additional bands of designed antenna are 2.35-2.91GHz,3.24-3.51GHz dielectric layers. But additional layers increase the weight of ,4.31-5.30GHz and 5.90-6.31GHz which is suitable for Bluetooth the antenna which is again undesirable in wireless (2.4GHZ),WLAN (2.4GHz,5.2GHz), WiMAX (2.3GHz, 2.5GHz, environment. -
A Layman's Interpretation Guide L-Band and C-Band Synthetic
A Layman’s Interpretation Guide to L-band and C-band Synthetic Aperture Radar data Version 2.0 15 November, 2018 Table of Contents 1 About this guide .................................................................................................................................... 2 2 Briefly about Synthetic Aperture Radar ......................................................................................... 2 2.1 The radar wavelength .................................................................................................................... 2 2.2 Polarisation ....................................................................................................................................... 3 2.3 Radar backscatter ........................................................................................................................... 3 2.3.1 Sigma-nought .................................................................................................................................................. 3 2.3.2 Gamma-nought ............................................................................................................................................... 3 2.4 Backscatter mechanisms .............................................................................................................. 4 2.4.1 Direct backscatter ......................................................................................................................................... 4 2.4.2 Forward scattering ...................................................................................................................................... -
Satellite Communications
Satellite Communications Ashaad Rambharos CSE, Intelsat 1 Satellite Example IS904 • General Satellite Information • Spacecraft Type: Three-Axis Stabilized • Orbital Location: 60.0 ° East Longitude • Orbital Control: +/- 0.05 ° • Launch: 23 February 2002 2 IS904 Coverage maps 3 General Satellite Information cont • Payload: Up to 34 x 72 MHz C-Band transponders * • Up to 11 x 36 MHz C-Band transponders * • 2 x 41 MHz C-Band transponders • Up to 2 x 77 MHz Ku-Band transponders • Up to 6 x 72 MHz Ku-Band transponders • Up to 8 x 36 MHz Ku-Band transponders • Frequency Bands: • C-Band: Uplink 5850 – 6425 MHz • Downlink 3625 – 4200 MHz • Ku-Band: Uplink 14.00 – 14.50 GHz • Downlink 10.95 – 11.20 GHz (Band A) and • Downlink 11.45 – 11.70 GHz (Band B) • Beacons: • 3947.5 or 3948 MHz 3952 or 3952.5 MHz • 11198 MHz 11452 MHz 4 Intelsat 904 C-Band Payload • Number of Transponders: • Up to 34 x 72 MHz * • Up to 11 x 36 MHz * • 2 x 41 MHz • Transponder Bandwidth: • 72 MHz with 8 MHz Guard Bands • 36 MHz with 4 MHz Guard Bands • 41 MHz with 4 MHz Guard Bands • Polarization: Circular: LHCP and RHCP • SFD (at Beam Reference Contour): -67.0 to -89.0 dBW/m² • Input Attenuators: 22 dB in 2 dB steps • 5 Intelsat 904 C-Band Payload cont • G/T: > -11.2 dB/K typical for GA, GB > -7.4 dB/K typical for WH > -5.1 dB/K typical for EH > 0.0 dB/K typical for NWZ > -1.5 dB/K typical for NEZ, SEZ > -3.5 dB/K typical for MEZ > -5.0 dB/K typical for SWZ > -4.5 dB/K typical for CEZ (combined NEZ/SEZ) • EIRP: > 31.0 dBW typical for GA, GB > 40.1 dBW typical for Ch. -
Wide-Band, Low-Frequency Pulse Profiles of 100 Radio Pulsars With
A&A 586, A92 (2016) Astronomy DOI: 10.1051/0004-6361/201425196 & c ESO 2016 Astrophysics Wide-band, low-frequency pulse profiles of 100 radio pulsars with LOFAR M. Pilia1,2, J. W. T. Hessels1,3,B.W.Stappers4, V. I. Kondratiev1,5,M.Kramer6,4, J. van Leeuwen1,3, P. Weltevrede4, A. G. Lyne4,K.Zagkouris7, T. E. Hassall8,A.V.Bilous9,R.P.Breton8,H.Falcke9,1, J.-M. Grießmeier10,11, E. Keane12,13, A. Karastergiou7 , M. Kuniyoshi14, A. Noutsos6, S. Osłowski15,6, M. Serylak16, C. Sobey1, S. ter Veen9, A. Alexov17, J. Anderson18, A. Asgekar1,19,I.M.Avruch20,21,M.E.Bell22,M.J.Bentum1,23,G.Bernardi24, L. Bîrzan25, A. Bonafede26, F. Breitling27,J.W.Broderick7,8, M. Brüggen26,B.Ciardi28,S.Corbel29,11,E.deGeus1,30, A. de Jong1,A.Deller1,S.Duscha1,J.Eislöffel31,R.A.Fallows1, R. Fender7, C. Ferrari32, W. Frieswijk1, M. A. Garrett1,25,A.W.Gunst1, J. P. Hamaker1, G. Heald1, A. Horneffer6, P. Jonker20, E. Juette33, G. Kuper1, P. Maat1, G. Mann27,S.Markoff3, R. McFadden1, D. McKay-Bukowski34,35, J. C. A. Miller-Jones36, A. Nelles9, H. Paas37, M. Pandey-Pommier38, M. Pietka7,R.Pizzo1,A.G.Polatidis1,W.Reich6, H. Röttgering25, A. Rowlinson22, D. Schwarz15,O.Smirnov39,40, M. Steinmetz27,A.Stewart7, J. D. Swinbank41,M.Tagger10,Y.Tang1, C. Tasse42, S. Thoudam9,M.C.Toribio1,A.J.vanderHorst3,R.Vermeulen1,C.Vocks27, R. J. van Weeren24, R. A. M. J. Wijers3, R. Wijnands3, S. J. Wijnholds1,O.Wucknitz6,andP.Zarka42 (Affiliations can be found after the references) Received 20 October 2014 / Accepted 18 September 2015 ABSTRACT Context. -
Considerations and Strategies for Maximizing C-Band Deployment
Considerations and Strategies for Maximizing C-band Deployment Solutions and Best Practices Contents Abstract . 3 Introduction . 3 Beamforming. 4 Site Architecture ............................................................. 6 Coexistence with FSS. 7 Supply Power ................................................................ 8 Small Cells. 8 Fronthaul and Backhaul ...................................................... 10 Summary. 11 2 Considerations and Strategies for Maximizing C-band Deployment - Solutions and Best Practices Abstract The recently concluded C-band auction has created new opportunities to help mobile operators address the ever- growing need for network capacity, spectral efficiency and a migration path to 5G and beyond. As with all mobile technology innovations, the benefits the new C-band spectrum provides will depend on how operators plan for and implement it into their existing legacy networks. There are a number of key challenges, including the integration of advanced beamforming technologies, the rise of massive and multi-user MIMO, site architecture issues, potential interference with fixed satellite services and use with small cells, to name a few. This white paper provides a wide- angle perspective of some of the major challenges facing operators as they consider the strategies for deploying new C-band capabilities. It also shines a light on some of the innovative developments from leading network OEMs like CommScope. Introduction As we begin 2021, the first commercial 5G networks are well in 46 major markets in late 2021. The remaining 180 MHz over a year into operation. During the past year, 5G activities (3.8–3.98 GHz) will be added nationwide in a second phase on a have accelerated and now outpace the growth rate of all past timeline to be agreed upon by the parties in each market. -
An Elementary Approach Towards Satellite Communication
AN ELEMENTARY APPROACH TOWARDS SATELLITE COMMUNICATION Prof. Dr. Hari Krishnan GOPAKUMAR Prof. Dr. Ashok JAMMI AN ELEMENTARY APPROACH TOWARDS SATELLITE COMMUNICATION Prof. Dr. Hari Krishnan GOPAKUMAR Prof. Dr. Ashok JAMMI AN ELEMENTARY APPROACH TOWARDS SATELLITE COMMUNICATION WRITERS Prof. Dr. Hari Krishnan GOPAKUMAR Prof. Dr. Ashok JAMMI Güven Plus Group Consultancy Inc. Co. Publications: 06/2021 APRIL-2021 Publisher Certificate No: 36934 E-ISBN: 978-605-7594-89-1 Güven Plus Group Consultancy Inc. Co. Publications All kinds of publication rights of this scientific book belong to GÜVEN PLUS GROUP CONSULTANCY INC. CO. PUBLICATIONS. Without the written permission of the publisher, the whole or part of the book cannot be printed, broadcast, reproduced or distributed electronically, mechanically or by photocopying. The responsibility for all information and content in this Book, visuals, graphics, direct quotations and responsibility for ethics / institutional permission belongs to the respective authors. In case of any legal negativity, the institutions that support the preparation of the book, especially GÜVEN PLUS GROUP CONSULTANCY INC. CO. PUBLISHING, the institution (s) responsible for the editing and design of the book, and the book editors and other person (s) do not accept any “material and moral” liability and legal responsibility and cannot be taken under legal obligation. We reserve our rights in this respect as GÜVEN GROUP CONSULTANCY “PUBLISHING” INC. CO. in material and moral aspects. In any legal problem/situation TURKEY/ISTANBUL courts are authorized. This work, prepared and published by Güven Plus Group Consultancy Inc. Co., has ISO: 10002: 2014- 14001: 2004-9001: 2008-18001: 2007 certificates. This work is a branded work by the TPI “Turkish Patent Institute” with the registration number “Güven Plus Group Consultancy Inc. -
Potential of Different Optical and SAR Data in Forest and Land Cover Classification to Support REDD+ MRV
remote sensing Article Potential of Different Optical and SAR Data in Forest and Land Cover Classification to Support REDD+ MRV Laura Sirro 1,*, Tuomas Häme 1, Yrjö Rauste 1, Jorma Kilpi 1 ID , Jarno Hämäläinen 2, Katja Gunia 2, Bernardus de Jong 3 and Fernando Paz Pellat 4 1 VTT Technical Research Centre of Finland Ltd., P.O. Box 1000, VTT FI-02044, Finland; tuomas.hame@vtt.fi (T.H.); yrjo.rauste@vtt.fi (Y.R.); jorma.kilpi@vtt.fi (J.K.) 2 Arbonaut Ltd., Kaislakatu 2, Joensuu FI-80130, Finland; [email protected] (J.H.); [email protected] (K.G.) 3 El Colegio de la Frontera Sur, Av. Rancho Polígono 2-A, Parque Industrial Lerma, Campeche, Campeche CP 24500, Mexico; [email protected] 4 Colegio de Postgraduados, Km 36.5 Carretera México-Texcoco, Texcoco 56230, Mexico; [email protected] * Correspondence: laura.sirro@vtt.fi; Tel.: +358-40-538-7769 Received: 9 May 2018; Accepted: 11 June 2018; Published: 14 June 2018 Abstract: The applicability of optical and synthetic aperture radar (SAR) data for land cover classification to support REDD+ (Reducing Emissions from Deforestation and Forest Degradation) MRV (measuring, reporting and verification) services was tested on a tropical to sub-tropical test site. The 100 km by 100 km test site was situated in the State of Chiapas in Mexico. Land cover classifications were computed using RapidEye and Landsat TM optical satellite images and ALOS PALSAR L-band and Envisat ASAR C-band images. Identical sample plot data from Kompsat-2 imagery of one-metre spatial resolution were used for the accuracy assessment. -
Raytheon Missile Systems Application to Renew WF2XLI File No: 0036-EX-CR-2017
Raytheon Missile Systems Application to Renew WF2XLI File No: 0036-EX-CR-2017 Explanation of Experiments and Need for Experimental License for use of Several Frequency Bands for Lab and Factory Missile Communications Testing Overview: Raytheon Missile Systems builds and sells missiles to the US military. As a part of the engineering development and production process, RMS tests communications systems in its products to make sure they meet customer specifications. Currently, RMS holds a license for operations in Tucson, Arizona and Camden, Arkansas, WF2XLI, for the ongoing operations it is requesting to renew. The ongoing experimental operations are for testing command and control systems in the lab and for factory missile communications testing. The four radio systems are used in the field by Raytheon’s customers for Range Safety. The four radio systems used for testing are the Flight Terminate Receiver (UHF), the L- band telemetry transmitter, the S-Band telemetry transmitter, and the C-Band transponder. These systems must be tested and retested as part of the production process for the Range Flight Safety System. This license uses the systems installed on missiles that will be tested at government ranges. Prior to delivery of the product to the customer, the product must be tested as part of engineering development and production testing. The actual missile flight testing is conducted at government test and training ranges using federal frequency assignments. Since the lab and production testing is ongoing at Raytheon’s facilities, and because some of the work being done is actually internal to Raytheon as part of independent research and development, it is necessary to renew this experimental authorization to allow for the proper, licensed operation of the missile during development and production testing. -
VHF and L-Band Scintillation Characteristics Over an Indian Low Latitude Station, Waltair (17.7◦ N, 83.3◦ E)
Annales Geophysicae, 23, 2457–2464, 2005 SRef-ID: 1432-0576/ag/2005-23-2457 Annales © European Geosciences Union 2005 Geophysicae VHF and L-band scintillation characteristics over an Indian low latitude station, Waltair (17.7◦ N, 83.3◦ E) P. V. S. Rama Rao, S. Tulasi Ram, K. Niranjan, D. S. V. V. D. Prasad, S. Gopi Krishna, and N. K. M. Lakshmi Space Physics Laboratories, Department of Physics, Andhra University, Visakhapatnam 530 003, India Received: 30 April 2005 – Revised: 6 August 2005 – Accepted: 10 August 2005 – Published: 14 October 2005 Abstract. Characteristics of simultaneous VHF (244 MHz) tures in the Range-Time-Intensity (RTI) images of HF radars, and L-band (1.5 GHz) scintillations recorded at a low- intensity bite-outs in airglow intensity measurements and latitude station, Waltair (17.7◦ N, 83.3◦ E), during the low scintillations on amplitude, as well as the phase of VHF and sunspot activity year of March 2004 to March 2005, sug- UHF signals from satellites, and are commonly referred to as gest that the occurrence of scintillations is mainly due to two Equatorial Spread-F irregularities (ESF). The ESF is mostly types, namely the Plasma Bubble Induced (PBI), which max- confined to the equatorial belt of ±20◦ magnetic latitudes, imizes during the post sunset hours of winter and equinoctial encompassing the Equatorial Ionization Anomaly (EIA) re- months, and the Bottom Side Sinusoidal (BSS) type, which gion. maximizes during the post-midnight hours of the summer Woodman and Lahoz (1976) classified the irregularities solstice