Repeaters, Satellites, EME and Direction Finding 23
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Naval Postgraduate School Petite Amateur Navy Satellite
f NAVAL POSTGRADUATE SCHOOL PETITE AMATEUR NAVY SATELLITE (PANSAT) NASA/USRA University Advanced Design Program i Final Design Report i L Summer 1989 Naval Postgraduate School Space Systems Academic Group Monterey, California (NA_A-CR-18_049) PETIT? AMATEUR NAVY N90-I1800 _TFLLIT_: (pANSAT) Find1 _eport (N_v;_i Postgrdduate School) ;1 o CSCL 22B ,i TABLE OF CONTENTS A. BACKGROUND ........................................................................... 2 B. DESIGN SUMMARY .................................................................... 3 1. Communications (COMM) ...................................................... 3 2. Data Processor & Sequencer (DP&S) ...................................... 3 Figure 1. PANSAT DP&S System Concept ................................................... 6 3. Power .................................................................................. 7 4. Structure Subsystem ............................................................... 8 Figure 2. PANSAT Structural Configuration .............................................. 10 5. Experiment Payload ............................................................. l0 ,, C. CONCLUSION ................................................... !........................ 11 [ APPENDIX ...................................................................... , ....................... 12 ! Fig. A1. Processor Main Board ................................................................. 12 Fig. A2. Telemetry Section, (A/D converters) ............................................ -
Real Time C Band Link Budget Model Calculation
REAL TIME C BAND LINK BUDGET MODEL CALCULATION Item Type text; Proceedings Authors Rubio, Pedro; Fernandez, Francisco; Jimenez, Francisco Publisher International Foundation for Telemetering Journal International Telemetering Conference Proceedings Rights Copyright © held by the author; distribution rights International Foundation for Telemetering Download date 27/09/2021 23:53:15 Link to Item http://hdl.handle.net/10150/624184 REAL TIME C BAND LINK BUDGET MODEL CALCULATION Pedro Rubio, Francisco Fernandez, Francisco Jimenez Airbus D&S - Flight Test 1. ABSTRACT The purpose of this paper is to show the integration of the transmission gain values of a telemetry transmission antenna according to its relative position and integrate them in the C band link budget, in order to obtain an accuracy vision of the link. Once our C band link budget was fully performed to model our link and ready to work in real time with several received values (GPS position, roll, pitch and yaw) from the aircraft and other values from the Ground System (azimuth and elevation of the reception telemetry antenna), it was necessary to avoid a constant value of the transmitter antenna and estimate its values with better accuracy depending of the relative beam angles between the transmitter antenna and receiver antenna. Keeping in mind an aircraft is not a static telecommunication system it was necessary to have a real time value of the transmission gain. In this paper, we will show how to perform a real time link budget (C band). Keywords: Telemetry, Link Budget, C band, Real time, Dynamic gain 2. WHY C BAND AND REAL TIME – THE PREVIOUS SITUATION The new C Band migration involves the change of all telemetry chain and the challenge to cover the same area than in S Band with the same quality of service. -
Ssc09-Xii-03
SSC09-XII-03 The Promise of Innovation from University Space Systems: Are We Meeting It? Michael Swartwout St. Louis University 3450 Lindell Boulevard St. Louis, Missouri 63103; (314) 977-8240 [email protected] ABSTRACT A popular notion among universities is that we are innovation-drivers in the staid, risk-adverse spacecraft industry – we are to professional small satellites what small satellites are to the “battlestars”. By contrast, professional industry takes a much different perspective on university-class spacecraft; these programs are good for attracting students to space and providing valuable pre-career training, but the actual flight missions are ancillary, even unimportant. Which opinion is correct? Both are correct. The vast majority of the 111 student-built spacecraft that have flown have made no innovative contributions. That is not to say that they have been without contribution. In addition to the inarguable benefits to education, many have served as radio Amateur communications, science experiments and even technological demonstrations. But “innovative”? Not so much. However, there have been two innovative contributors, whose contributions are large enough to settle the question: the University of Surrey begat SSTL, which helped create the COTS-based small satellite industry. Stanford and Cal Poly begat CubeSats, whose contributions are still being created today. This paper provides an update to our earlier submissions on the history of student-built spacecraft. Major trends identified in previous years will be re-examined with new data -- especially the bifurcation between larger-scale, larger-scope "flagship" programs and small-scale, reduced-mission "independents". In particular, we will demonstrate that the general history of student-built spacecraft has not been one of innovation, nor of development of new space systems -- with those few, extremely noteworthy, exceptions. -
ECE145C: RF CMOS Communication Circuits and Systems Prof
ECE145C: RF CMOS Communication Circuits and Systems Prof. James Buckwalter © James Buckwalter 1 Organization • email: [email protected] • Lecture: Girvetz Hall 1112 8-9:15 • Faq: Piazza access code: ece145c (Gauchospace?) • Please allow 24-48 hour turnaround • Computing Lab: E1 • TAs – Di Li • Office Hours: T/Th 12-1, TBD • OH Location: ESB-2205C © James Buckwalter 2 Scope: ECE 145C should • refine fundamental understanding of RF circuits and systems to analyze modern wireless technology. • present a comprehensive understanding from devices to systems. • teach applications of RF CMOS as well as III-V • analyze RF transmitter/receiver architectures. Modern cellular and RF technologies are a mash-up of communication theory and devices. One needs to understand device limitations to understand communication system limits and vice versa. © James Buckwalter 3 Topics for our class • Propagation, Noise and Distortion Budgeting • Basics of Modulation / Cellular Standards • Receiver Filtering, Mixing, and Architectures • Power Amplifiers (Linear and Nonlinear): Output power and Efficiency • High-efficiency transmitters • RF Architectures (Putting it all together) © James Buckwalter 4 Lecture Topic Lecture Topic 1 (3/31) System Perspective: 2 (4/2) System Perspective: Link Budget Interference 3 (4/7) System Perspective: EVM 4 (4/9) System Perspective: Reciprocal Mixing 5 (4/14) Mixers (1) 6 (4/16) Mixers(2) 7 (4/21) Tunable Filters (I) 8 (4/23) Midterm 9 (4/28) Tunable Filters (II) 10 (4/30) RX Architectures: Mixer First 11 (5/5) RX Architectures: Direct 12 (5/7) Power Amplifiers: Classes Sampling 13 (5/12) Power Amplifiers: Classes 14 (5/14) Power Amplifiers: Spectral Regrowth 15 (5/19) Outphasing 16 (5/21) Outphasing Modulators Modulators…Transmitters 17 (5/26) Doherty Transmitters 18 (5/28) Doherty Transmitters 19 (6/1) Envelope Tracking 20 (6/3) Midterm Transmitters Reference Material • Razavi…for now. -
Antenna Catalog. Volume 3. Ship Antennas
UNCLASSIFIED AD NUMBER AD323191 CLASSIFICATION CHANGES TO: unclassified FROM: confidential LIMITATION CHANGES TO: Approved for public release, distribution unlimited FROM: Distribution authorized to U.S. Gov't. agencies and their contractors; Administrative/Operational use; Oct 1960. Other requests shall be referred to Ari Force Cambridge Research Labs, Hansom AFB MA. AUTHORITY AFCRL Ltr, 13 Nov 1961.; AFCRL Ltr, 30 Oct 1974. THIS PAGE IS UNCLASSIFIED AD~ ~~~~~~O WIR1L_•_._,m,_, ANTENNA CATALOG Volume m UNCLASSIFIED SHIP ANTENN October 1960 Electronics Research Directorate AIR FORCE CAMBRIDGE RESEARCH LABORATORIES Can+rftc AT I9(6N4,4 101 by GEORGIA INSTITUTE OF TECHNOLOGY Engineering Experiment Station •o•log NOTIC 11ý4 Sadoqh amd P4is4,ej ww~aI~.. 1! d' ths, . 'to0 t,UL .. -+~~~~~-L#..-•...T... -w 0 I tdin #" "•: ..."- C UNCLASSIFIED AFCRC-TR-60-134(111) ANTENNA CATALOG Volume III SHIP ANTENNAS (Title UOwlnIied) October 1960 Appeoved: Mmurice W. Long, Electronics Division Submitteds A oed: Technical Information Section k Jeme,. L d, Directot Esis..ielng Expe•immnt Station Prepared by GEORGIA INSTITUTE OF TECHNOLOGY Engineering Experiment Station DOWNGRADED A-r 3 YEAR INTERVAIS. DECL~IFED AFTER 12 YEA&RS. DOD DIR 5200.10 UNC-LASSIFIED. , ~K-11. 574-1 ." TABLE OF CONTENTS Page INTRODUCTION . 1 EQUIPMENT FUNCTION ................ .................. ... 3 ANTENNA TYPE . 7 ANTENNA DATA AB Antennas ......... ................. .............. ...................... ... 15 AN Antennas ............................ ...................................... -
Path Loss and Link Budget
Path Loss and Link Budget Harald Welte <[email protected]> Path Loss A fundamental concept in planning any type of radio communications link is the concept of Path Loss. Path Loss describes the amount of signal loss (attenuation) between a receive and a transmitter. As GSM operates in frequency duplex on uplink and downlink, there is correspondingly an Uplink Path Loss from MS to BTS, and a Downlink Path Loss from BTS to MS. Both need to be considered. It is possible to compute the path loss in a theoretical ideal situation, where transmitter and receiver are in empty space, with no surfaces anywhere nearby causing reflections, and with no objects or materials in between them. This is generally called the Free Space Path Loss. Path Loss Estimating the path loss within a given real-world terrain/geography is a hard problem, and there are no easy solutions. It is impacted, among other things, by the height of the transmitter and receiver antennas whether there is line-of-sight (LOS) or non-line-of-sight (NLOS) the geography/terrain in terms of hills, mountains, etc. the vegetation in terms of attenuation by foliage any type of construction, and if so, the type of materials used in that construction, the height of the buildings, their distance, etc. the frequency (band) used. Lower frequencies generally expose better NLOS characteristics than higher frequencies. The above factors determine on the one hand side the actual attenuation of the radio wave between transmitter and receiver. On the other hand, they also determine how many reflections there are on this path, causing so-called Multipath Fading of the signal. -
PANSAT) Was Launched Aboard the STS-95 Discovery Shuttle
777 Dyer Rd., Rm. 125, Code (SP/Sd), Monterey, California 93943 (831) 656-2299; email: [email protected] Abstract. The Petite Amateur Navy Satellite (PANSAT) was launched aboard the STS-95 Discovery Shuttle. The hist flight noted mainly by John Glenn’s return to space also marks the Naval Postgraduate School’s first smal space. PANSAT, which is in a circular, low-Earth orbit (LEO), is the culmination of 50 officer studen theses over approximately a nine-year period. The satellite continues to support the educational mission will soon provide on-orbit capability of store-and-forward digital communications for the amateur radio using direct sequence, spread spectrum modulation. The spacecraft includes the communications payloa power subsystem, digital control subsystem, and structure. This paper describes the overall architecture of th bus, a discussion of the NPS command ground station, and some lessons learned. Introduction Mission Requirements and Object The Space Systems Academic Group at NPS provides Education direction and a focal point for Naval Postgraduate School (NPS) space research and the space curricula: Space The primary objective for PANSAT is to pro Systems Engineering and Space Systems Operations. The on educational opportunities for the officer Petite Amateur Navy Satellite (PANSAT) is the first NPS NPS. The first phase of the program prov satellite in space. Approximately 50 Master’s degree support to the engineering disciplines through theses were published on the satellite. Officer students development, integration, and test. A numb played a vital role in the successful development of the were also related to operations. Now that satellite and gained invaluable experience through their operating in space, the emphasis has shift part in the project. -
Wireless Link Budget Analysis How to Calculate Link Budget for Your Wireless Network
Wireless Link Budget Analysis How to Calculate Link Budget for Your Wireless Network Whitepaper Radio Systems How far can it go and what will the throughput be? These are the two common questions that come up when designing a high speed wireless data link. There are several factors that may impact the performance of a radio system. Available and permitted output power, available bandwidth, receiver sensitivity, antenna gains, radio technology, and environmental conditions are some of the major factors that may impact system performance. For large scale network deployments, a detailed site survey and network design are highly recommended. This paper will attempt to provide the reader with an overview on how a link budget is calculated. Line-of-Sight (LOS) Link Budget To limit the scope of this paper, only line-of-sight links with sufficient Fresnel Zone clearance will be considered. The following equation shows the basic elements that need to considered when calculating a link budget: Received Power (dBm) = Transmitted Power (dBm) + Gains (dB) − Losses (dB) If the estimated received power is sufficiently large (typically relative to the receiver sensitivity), the link budget is said to be sufficient for sending data under perfect conditions. The amount by which the received power exceeds receiver sensitivity is FSPL (dB) called the link margin . Distance 900MHz 2.4GHz 5.8GHz 1km Free-Space Path Loss 91.53 100.05 107.72 2km 97.56 106.07 113.74 In a line-of-sight radio system, losses are mainly due to free-space path loss (FSPL ). FSPL is proportional to the square of the distance between the transmitter and 3km 101.08 109.60 117.26 receiver as well as the square of the frequency of the radio signal. -
The Petite Amateur Navy Satellite (PANSAT) Hitchhiker Ejectable
View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by Calhoun, Institutional Archive of the Naval Postgraduate School Calhoun: The NPS Institutional Archive Faculty and Researcher Publications Faculty and Researcher Publications Collection 1998 The Petite Amateur Navy Satellite (PANSAT) Hitchhiker Ejectable Sakoda, Daniel Monterey, California: Naval Postgraduate School. http://hdl.handle.net/10945/37436 THE PETITE AMATEUR NAVY SATELLITE (PANSAT) HITCHHIKER EJECTABLE Daniel Sakoda Aerospace Engineer, Naval Postgraduate School ABSTRACT The Petite Amateur Navy Satellite (PANSAT) was successfully launched aboard the STS- 95 Discovery Shuttle as part of the third International Extreme Ultraviolet Hitchhiker (IEH-3), and placed into a circular, low-Earth orbit with 555 km (300 nmi.) altitude and 28.5° inclination. The culmination of approximately 50 graduate student theses, PANSAT provides the amateur radio community with digital, store-and-forward, direct sequence, spread spectrum communications, as well as providing officer students at NPS a space-based instructional laboratory. The spacecraft hardware was built and tested almost entirely at NPS to the component level. Rigorous analysis and testing was performed to ensure compatibility with Shuttle payload requirements. This paper describes the spacecraft design as relates to both compliance with Shuttle safety requirements and ensuring overall mission success. Specifically, PANSAT design requirements for structures, radio frequency emissions, and batteries will be discussed along with some lessons learned in the verification process. INTRODUCTION The Petite Amateur Navy Satellite (PANSAT) is the Naval Postgraduate School's (NPS) first satellite in space. The main objective is to provide a hands-on, educational tool for the officer students at NPS in the Space Systems Engineering and Space Systems Operations curricula. -
AN1631-Simple Link Budget Estimation and Performance
AN1631 Simple Link Budget Estimation and Performance Measurements of Microchip Sub-GHz Radio Modules Usually, Sub-GHz channels are part of unlicensed Author: Pradeep Shamanna Industrial Scientific Medical (ISM) frequency bands. Microchip Technology Inc. Sub-GHz nodes generally target low-cost systems, with each node costing approximately 30% to 40% less compared to the advanced wireless systems and uses INTRODUCTION less stack memory. Many protocols such as IEEE ® The increased popularity of short range wireless in 802.15.4 based ZigBee (currently, the only protocol home, building and industrial applications with Sub- offering both 2.4 GHz and Sub-GHz versions in the GHz (<1 GHz) band requires the system designers to 868 MHz and 900 MHz bands), automation protocols, understand the methods, estimation, cost and trade-off cordless phones, Wireless Modbus, Remote Keyless in short range wireless communication. Apart from Entry (RKE), Tire Pressure Monitoring System (TPMS) considering the range estimation formula, it is good to and lot of proprietary protocols (including MiWi™), understand the wireless channel and propagation occupy this band. However, operation in the Sub-GHz environment involved with Sub-GHz. Generally, RF/ ISM band induces the radios to interfere with other wireless engineers perform a link budget while starting protocols utilizing the same spectrum which includes an RF design. The link budget considers range, threat from mobile phones, licensed cordless phones, transmit power, receiver sensitivity, antenna gains, and so on. frequency, reliability, propagation medium (which This application note describes a simple link budget includes the principles of physics linked to reflection, analysis, measurement and techniques to evaluate the diffraction and scattering of electromagnetic waves), range and performance of wireless transmission with and environment factors to accurately calculate the results, and uses developed models to estimate the performance of a Sub-GHz RF radio link. -
Some of the Women of Goddard Involved in the Space Shuttle
Space Shuttle Discovery, March 7, 2011, as photographed from the International Space Station. Space Shuttle: A Key to NASA’s Space Transportation System Following the spectacular successes of the Apollo program, NASA designed the Space Transportation System (STS), including the crew-tended Space Shuttle orbiter, to provide a reusable vehicle for launching heavy payloads, maintaining low Earth orbit, and returning to ground with a runway landing. The Shuttle made its first orbital flight in April 1981 and its last flight in July 2011. The manifests for Space Shuttle Endeavour, making its final landing at Kennedy Space Center, the 135 flights were very diverse, from deploying planetary spacecraft June 1, 2011. and servicing the Hubble Space Telescope to construction of the International Space Station in low Earth orbit. The Shuttle program is centered at NASA’s Johnson Space Center and Kennedy Space Center, but it has important NASA Goddard Space Flight Center contributions. Astronaut Mary Cleave conducting an experiment on Space Shuttle Atlantis in May 1989. A rare event with two Space Shuttle Orbiters (Atlantis and Endeavour) simultaneously being prepared for separate launches at Kennedy Space Center, September 20, 2008. Photo by Jack Pfaller Space Shuttle Atlantis, July 8, 2011, lifting off with its four-member crew on the Shuttle program’s final mission. International Space Station Freedom, a laboratory dedicated to humans living and working in Low Earth Orbit, March 7, 2011, as The edge of the Earth’s atmosphere on photographed from -
Range Calculation for 300Mhz to 1000Mhz Communication Systems
APPLICATION NOTE Range Calculation for 300MHz to 1000MHz Communication Systems RANGE CALCULATION Description For restricted-power UHF* communication systems, as defined in FCC Rules and Regula- tions Title 47 Part 15 Subpart C “intentional radiators*”, communication range capability is a topic which generates much interest. Although determined by several factors, communica- tion range is quantified by a surprisingly simple equation developed in 1946 by H.T. Friis of Denmark. This paper begins by introducing the Friis Transmission Equation and examining the terms comprising it. Then, real-world-environment factors which influence RF commu- nication range and how they affect a “Link Budget*” are investigated. Following that, some methods for optimizing RF-link range are given. Range-calculation spreadsheets, including the special case of RKE, are presented. Finally, information concerning FCC rules govern- ing “intentional radiators”, FCC-established radiation limits, and similar reference material is provided. Section 7. “Appendix” on page 13 includes definitions (words are marked with an asterisk *) and formulas. Note: “For additional information, two excel spreadsheets, RKE Range Calculation (MF).xls and Generic Range Calculation.xls, have been attached to this PDF. To open the attachments, in the Attachments panel, select the attachment, and then click Open or choose Open Attachment from the Options menu. For addi- tional information on attachments, please refer to Adobe Acrobat Help menu“ 9144C-RKE-07/15 1. The Friis Transmission Equation For anyone using a radio to communicate across some distance, whatever the type of communication, range capability is inevitably a primary concern. Whether it is a cell-phone user concerned about dropped calls, kids playing with their walkie- talkies, a HAM radio operator with VHF/UHF equipment providing emergency communications during a natural disaster, or a driver opening a garage door from their car in the pouring rain, an expectation for reliable communication always exists.