A TIME-DIVISION MULTIPLEXING SYSTEM for ASYNCHRONOUS HIGH-RATE TELEMETRY R
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Design and Evaluation of a Clock Multiplexing Circuit for the SSRL Booster Accelerator Timing System
SLAC-TN-15-018 Design and Evaluation of a Clock Multiplexing Circuit for the SSRL Booster Accelerator Timing System Million Araya† August 21, 2015 Seattle Central Community College, Seattle, WA CCI Program, SLAC National Accelerator Laboratory SPEAR3 is a 234 m circular storage ring at SLAC’s synchrotron radiation facility (SSRL) in which a 3 GeV electron beam is stored for user access. Typically the electron beam decays with a time constant of approximately 10hr due to electron lose. In order to replenish the lost electrons, a booster synchrotron is used to accelerate fresh electrons up to 3GeV for injection into SPEAR3. In order to maintain a constant electron beam current of 500mA, the injection process occurs at 5 minute intervals. At these times the booster synchrotron accelerates electrons for injection at a 10Hz rate. A 10Hz 'injection ready' clock pulse train is generated when the booster synchrotron is operating. Between injection intervals-where the booster is not running and hence the 10 Hz ‘injection ready’ signal is not present-a 10Hz clock is derived from the power line supplied by Pacific Gas and Electric (PG&E) to keep track of the injection timing. For this project I constructed a multiplexing circuit to 'switch' between the booster synchrotron 'injection ready' clock signal and PG&E based clock signal. The circuit uses digital IC components and is capable of making glitch-free transitions between the two clocks. This report details construction of a prototype multiplexing circuit including test results and suggests improvement opportunities for the final design. I. Introduction The ultimate purpose of a synchrotron radiation facility is to generate stable, high-power beams of light spanning from the Infrared to x-ray portion of the electromagnetic spectrum. -
Communications
The Essentials of Datalink Communications The origins and course of Air-to-Ground Messaging The Essentials of Datalink Communications Contents international Trip Support | international Trip The Technology that HR Created 02 Inmarsat Satellite 06 Growing into an Operational Necessity 03 Iridium Satellite 07 UAS Communications Mechanisms 04 Upcoming Regulations 10 VHF Radio 05 The Future of ACARS 11 © Copyright 2016 Page 1/12 The Technology that HR Created t one time in the not-so-distant past, pilots and other ARINC’s solution was an automated system, called the A flight crew members were paid different rates for the ARINC Communications Addressing and Reporting System, time they were airborne versus the time they were performing or ACARS for short, which sent short text data from the ground operations. Events like aircraft pushback, taxi, takeoff, avionics of the aircraft directly to the ground-based entities landing, and gate arrival were transmitted via voice over radio through Very High Frequency (VHF) radio frequencies frequencies to operators who would relay this information back without any crewmember involvement. The aircraft was to the airlines. The pilots were responsible for self-reporting programmed to take advantage of switches and automation their own times and movements. Understanding that people points on the aircraft, resulting in the creation of a set of can sometimes be forgetful, or worse, willfully manipulative, messages referred to as the OOOI report. An OOOI report is the major airlines began searching for a solution that tracked any of four messages: Out, Off, On and In. Still in wide-scale crewmember pay in a more structured and accurate way. -
Data Networks
Second Ed ition Data Networks DIMITRI BERTSEKAS Massachusetts Institute of Technology ROBERT GALLAGER Massachusetts Institute ofTechnology PRENTICE HALL, Englewood Cliffs, New Jersey 07632 2 Node A Node B Time at B --------- Packet 0 Point-to-Point Protocols and Links 2.1 INTRODUCTION This chapter first provides an introduction to the physical communication links that constitute the building blocks of data networks. The major focus of the chapter is then data link control (i.e., the point-to-point protocols needed to control the passage of data over a communication link). Finally, a number of point-to-point protocols at the network, transport, and physical layers are discussed. There are many similarities between the point-to-point protocols at these different layers, and it is desirable to discuss them together before addressing the more complex network-wide protocols for routing, flow control, and multiaccess control. The treatment of physical links in Section 2.2 is a brief introduction to a very large topic. The reason for the brevity is not that the subject lacks importance or inherent interest, but rather, that a thorough understanding requires a background in linear system theory, random processes, and modem communication theory. In this section we pro vide a sufficient overview for those lacking this background and provide a review and perspective for those with more background. 37 38 Point-to-Point Protocols and Links Chap. 2 In dealing with the physical layer in Section 2.2, we discuss both the actual com munication channels used by the network and whatever interface modules are required at the ends of the channels to transmit and receive digital data (see Fig 2.1). -
Radio Communications in the Digital Age
Radio Communications In the Digital Age Volume 1 HF TECHNOLOGY Edition 2 First Edition: September 1996 Second Edition: October 2005 © Harris Corporation 2005 All rights reserved Library of Congress Catalog Card Number: 96-94476 Harris Corporation, RF Communications Division Radio Communications in the Digital Age Volume One: HF Technology, Edition 2 Printed in USA © 10/05 R.O. 10K B1006A All Harris RF Communications products and systems included herein are registered trademarks of the Harris Corporation. TABLE OF CONTENTS INTRODUCTION...............................................................................1 CHAPTER 1 PRINCIPLES OF RADIO COMMUNICATIONS .....................................6 CHAPTER 2 THE IONOSPHERE AND HF RADIO PROPAGATION..........................16 CHAPTER 3 ELEMENTS IN AN HF RADIO ..........................................................24 CHAPTER 4 NOISE AND INTERFERENCE............................................................36 CHAPTER 5 HF MODEMS .................................................................................40 CHAPTER 6 AUTOMATIC LINK ESTABLISHMENT (ALE) TECHNOLOGY...............48 CHAPTER 7 DIGITAL VOICE ..............................................................................55 CHAPTER 8 DATA SYSTEMS .............................................................................59 CHAPTER 9 SECURING COMMUNICATIONS.....................................................71 CHAPTER 10 FUTURE DIRECTIONS .....................................................................77 APPENDIX A STANDARDS -
Global Operational Data Link Document (GOLD)
Global Operational Data Link Document (GOLD) This edition has been issued by the GOLD ad hoc Working Group for the Asia/Pacific Air Navigation Planning and Implementation Regional Group (APANPIRG), the North Atlantic Systems Planning Group (NAT SPG), the European Air Navigation Planning Group (EANPG), the South American Region Implementation Group (SAM/IG) and the African-Indian Ocean Planning and Implementation Regional Group (APIRG). Second Edition — 26 April 2013 International Civil Aviation Organization GOLD (1) Second Edition — 26 April 2013 This document is available by accessing any of the following ICAO regional websites. Asia and Pacific (APAC) Office http://www.icao.int/apac Eastern and Southern African (ESAF) Office www.icao.int/esaf European and North Atlantic (EUR/NAT) Office http://www.paris.icao.int Middle East (MID) Office www.icao.int/mid North American, Central American and Caribbean (NACC) Office http://www.mexico.icao.int South American (SAM) Office http://www.lima.icao.int Western and Central African (WACAF) Office http://www.icao.int/wacaf For more information, contact the ICAO regional office. Global Operational Data Link Document (GOLD) This edition has been issued by the GOLD ad hoc Working Group for the Asia/Pacific Air Navigation Planning and Implementation Regional Group (APANPIRG), the North Atlantic Systems Planning Group (NAT SPG), the European Air Navigation Planning Group (EANPG), the South American Region Implementation Group (SAM/IG) and the African-Indian Ocean Planning and Implementation Regional Group (APIRG). Second Edition — 26 April 2013 International Civil Aviation Organization GOLD (i) Second Edition — 26 April 2013 (ii) Global Operational Data Link Document (GOLD) AMENDMENTS The issue of amendments is announced by the ICAO Regional Offices concerned, which holders of this publication should consult. -
V850 Standby Modes
Application Note V850 Standby Modes V850ES/SG2 V850ES/SJ2 Document No. U18825EE1V0AN00 Date Published June 2007 © NEC Electronics Corporation June 2007 Printed in Germany NOTES FOR CMOS DEVICES 1 VOLTAGE APPLICATION WAVEFORM AT INPUT PIN Waveform distortion due to input noise or a reflected wave may cause malfunction. If the input of the CMOS device stays in the area between VIL (MAX) and VIH (MIN) due to noise, etc., the device may malfunction. Take care to prevent chattering noise from entering the device when the input level is fixed, and also in the transition period when the input level passes through the area between VIL (MAX) and VIH (MIN). 2 HANDLING OF UNUSED INPUT PINS Unconnected CMOS device inputs can be cause of malfunction. If an input pin is unconnected, it is possible that an internal input level may be generated due to noise, etc., causing malfunction. CMOS devices behave differently than Bipolar or NMOS devices. Input levels of CMOS devices must be fixed high or low by using pull-up or pull-down circuitry. Each unused pin should be connected to VDD or GND via a resistor if there is a possibility that it will be an output pin. All handling related to unused pins must be judged separately for each device and according to related specifications governing the device. 3 PRECAUTION AGAINST ESD A strong electric field, when exposed to a MOS device, can cause destruction of the gate oxide and ultimately degrade the device operation. Steps must be taken to stop generation of static electricity as much as possible, and quickly dissipate it when it has occurred. -
Generate a Clock Signal from a Crystal Oscillator
www.ti.com Product Overview Generate a Clock Signal from a Crystal Oscillator Clocked Device U CLK Figure 1-1. Using an Unbuffered Inverter and Schmitt-Trigger Inverter to Generate a Clock Signal From a Crystal Oscillator Design Considerations • Drive crystal oscillators directly • Can be disabled with added logic • Allows for selectable system clocks with multiple crystals • Outputs a clean and reliable square wave • See the Use of the CMOS Unbuffered Inverter in Oscillator Circuits Application Report for more information about this use case. • Need additional assistance? Ask our engineers a question on the TI E2E™ logic support forum Recommended Parts Part Number Automotive Qualified VCC Range Features SN74LVC2GU04-Q1 ✓ 1.65 V — 5.5 V Dual unbuffered inverter SN74LVC2GU04 SN74AHC1GU04 2 V — 5.5 V Single unbuffered inverter SN74AUC1GU04 0.8 V — 2.7 V Single unbuffered inverter SN74LVC1G17-Q1 ✓ 1.65 V — 5.5 V Single Schmitt-trigger buffer SN74LVC1G17 For more devices, browse through the online parametric tool where you can sort by desired voltage, channel numbers, and other features. SCEA099 – OCTOBER 2020 Generate a Clock Signal from a Crystal Oscillator 1 Submit Document Feedback Copyright © 2020 Texas Instruments Incorporated IMPORTANT NOTICE AND DISCLAIMER TI PROVIDES TECHNICAL AND RELIABILITY DATA (INCLUDING DATASHEETS), DESIGN RESOURCES (INCLUDING REFERENCE DESIGNS), APPLICATION OR OTHER DESIGN ADVICE, WEB TOOLS, SAFETY INFORMATION, AND OTHER RESOURCES “AS IS” AND WITH ALL FAULTS, AND DISCLAIMS ALL WARRANTIES, EXPRESS AND IMPLIED, INCLUDING WITHOUT LIMITATION ANY IMPLIED WARRANTIES OF MERCHANTABILITY, FITNESS FOR A PARTICULAR PURPOSE OR NON-INFRINGEMENT OF THIRD PARTY INTELLECTUAL PROPERTY RIGHTS. These resources are intended for skilled developers designing with TI products. -
VLSI Digital Signal Processing
CLOCKS Clocks in Digital Systems • Why are clocks and clocked memory registers needed inside digital systems? • Clocks pace the flow of data inside digital processors • The exact speed of data through circuits is impossible to predict accurately due to factors such as: – Fabrication process variations – Supply voltage variations “PVT variations” – Temperature variations – Countless parasitic effects (e.g., wire-to-wire capacitances) – Data-dependent variations (e.g., calculating 1 OR 1 = 1 requires a different delay than 1 OR 0 = 1) © B. Baas 322 Clocks in Digital Systems • Clocked memory elements slow down the fastest signals, wait until all signals have finished propagating through the combinational logic in the stage*, and then release them into the next stage simultaneously, controlled by the active edge of the clock signal • * This is why we care about clock only the single slowest signal in a block (max propagation delay) when finding the maximum clock frequency © B. Baas 323 Clocks in Digital Systems • All paths within a digital system consist of an input register, (optionally) followed by combinational logic, followed by an output register • Therefore: – If we can make this structure work under all conditions, we can build a robust digital system – We should analyze this structure carefully clock a combinational out b logic c_p1 c_p3 © B. Baas c_p2 324 Robust Clock Design • Edge-triggered memory elements (flip-flops) are generally more robust than level-sensitive memory elements (transparent latches) • Always follow these rules in this class, and for the most robust designs: 1. Only clock signals may connect to flip-flop or latch clock inputs • A simpler circuit may sometimes be possible if a logic signal is connected to a clock input, but do not do it for robustness • always @(posedge key) begin 2. -
Tms320f280x, Tms320c280x, Tms320f2801x Digital Signal Processors
TMS320F2809, TMS320F2808, TMS320F2806, TMS320F2802, TMS320F2801, TMS320C2802, TMS320F2809, TMS320F2808, TMS320F2806,TMS320C2801, TMS320F2802, TMS320F28016, TMS320F2801, TMS320F28015TMS320C2802, www.ti.com TMS320C2801,SPRS230P – OCTOBER TMS320F28016, 2003 – REVISED TMS320F28015 FEBRUARY 2021 SPRS230P – OCTOBER 2003 – REVISED FEBRUARY 2021 TMS320F280x, TMS320C280x, TMS320F2801x digital signal processors 1 Features • Three 32-bit CPU timers • Enhanced control peripherals • High-performance static CMOS technology – Up to 16 PWM outputs – 100 MHz (10-ns cycle time) – Up to 6 HRPWM outputs with 150-ps MEP – 60 MHz (16.67-ns cycle time) resolution – Low-power (1.8-V core, 3.3-V I/O) design – Up to four capture inputs • JTAG boundary scan support – Up to two quadrature encoder interfaces – IEEE Standard 1149.1-1990 Standard Test – Up to six 32-bit/six 16-bit timers Access Port and Boundary Scan Architecture • Serial port peripherals • High-performance 32-bit CPU (TMS320C28x) – Up to 4 SPI modules – 16 × 16 and 32 × 32 MAC operations – Up to 2 SCI (UART) modules – 16 × 16 dual MAC – Up to 2 CAN modules – Harvard bus architecture – One Inter-Integrated-Circuit (I2C) bus – Atomic operations • 12-bit ADC, 16 channels – Fast interrupt response and processing – 2 × 8 channel input multiplexer – Unified memory programming model – Two sample-and-hold – Code-efficient (in C/C++ and Assembly) – Single/simultaneous conversions • On-chip memory – Fast conversion rate: – F2809: 128K × 16 flash, 18K × 16 SARAM 80 ns - 12.5 MSPS (F2809 only) F2808: 64K × 16 -
Phase Alignment of Asynchronous External
PHASEALIGNMENTOFASYNCHRONOUSEXTERNALCLOCK CONTROLLABLEDEVICESTOPERIODICMASTERCONTROLSIGNALUSING THEPERIODICEVENTSYNCHRONIZATIONUNIT by CharlesNicholasOstrander Athesissubmittedinpartialfulfillment oftherequirementsforthedegree of MasterofScience in ElectricalEngineering MONTANASTATEUNIVERSITY Bozeman,Montana May2009 ©COPYRIGHT by CharlesNicholasOstrander 2009 AllRightsReserved ii APPROVAL ofathesissubmittedby CharlesNicholasOstrander Thisthesishasbeenreadbyeachmemberofthethesiscommitteeandhasbeen foundtobesatisfactoryregardingcontent,Englishusage,format,citation,bibliographic style,andconsistency,andisreadyforsubmissiontotheDivisionofGraduateEducation. Dr.BrockJ.LaMeres ApprovedfortheDepartmentElectricalEngineering Dr.RobertC.Maher ApprovedfortheDivisionofGraduateEducation Dr.CarlA.Fox iii STATEMENTOFPERMISSIONTOUSE Inpresentingthisthesisinpartialfulfillmentoftherequirementsfora master’sdegreeatMontanaStateUniversity,IagreethattheLibraryshallmakeit availabletoborrowersunderrulesoftheLibrary. IfIhaveindicatedmyintentiontocopyrightthisthesisbyincludinga copyrightnoticepage,copyingisallowableonlyforscholarlypurposes,consistentwith “fairuse”asprescribedintheU.S.CopyrightLaw.Requestsforpermissionforextended quotationfromorreproductionofthisthesisinwholeorinpartsmaybegranted onlybythecopyrightholder. CharlesNicholasOstrander May2009 iv TABLEOFCONTENTS 1.INTRODUCTION .......................................................................................................... 1 -
Data Links Functions, Attributes and Latency
Nichols, Ryan, Mumm, Lonstein, & Carter Chapter 13: Data Links Functions, Attributes and Latency Student Learning Objectives The student will learn about the data-link function of the UAS which allows for bi-directional communication and data transmissions between UAV and its ground station. The Data Link is a vital component of an UAS. The student will learn the respective functions of each component part and considerations are necessary and how to evaluate their importance when developing a UAS. While the focus of the lesson will be on military applications, the considerations will be equally important for those designing and deploying UAS for civilian purposes. While the design of the Datalink must have requisite attributes that allow the system to function as intended in various environments globally, it must be able to do so securely and effectively. Issues such as Data Link security, interception, deception and signal latency are all attributes that must be balanced to achieve fast and secure data communications between the components of the UAS. What are the Types of UAV’s and how are they Categorized? UAV’s are most often divided into four categories based upon their mission duration and operational radius. High Altitude, Long Endurance (“HALE”) most often deployed for reconnaissance, interception or attack; Medium altitude, moderate range most often used for reconnaissance and combat effect assessment; Low cost, short range small UAV’s. (See Figure 13-1.) Components of the UAS Data-Link and their functions The UAV and Ground Control Station There are four essential communication and data processing operations the UAS must be able to efficiently and effectively carry out. -
7. Latches and Flip-Flops
Chapter 7 – Latches and Flip-Flops Page 1 of 18 7. Latches and Flip-Flops Latches and flip-flops are the basic elements for storing information. One latch or flip-flop can store one bit of information. The main difference between latches and flip-flops is that for latches, their outputs are constantly affected by their inputs as long as the enable signal is asserted. In other words, when they are enabled, their content changes immediately when their inputs change. Flip-flops, on the other hand, have their content change only either at the rising or falling edge of the enable signal. This enable signal is usually the controlling clock signal. After the rising or falling edge of the clock, the flip-flop content remains constant even if the input changes. There are basically four main types of latches and flip-flops: SR, D, JK, and T. The major differences in these flip-flop types are the number of inputs they have and how they change state. For each type, there are also different variations that enhance their operations. In this chapter, we will look at the operations of the various latches and flip- flops. 7.1 Bistable Element The simplest sequential circuit or storage element is a bistable element, which is constructed with two inverters connected sequentially in a loop as shown in Figure 1. It has no inputs and two outputs labeled Q and Q’. Since the circuit has no inputs, we cannot change the values of Q and Q’. However, Q will take on whatever value it happens to be when the circuit is first powered up.