Army Aviation Enabling The Future While Performing Today
|
|
|
- Marion Briggs
- 6 years ago
- Views:
Transcription
1 Army Aviation Enabling The Future While Performing Today ASN-128D - Future Impacts of the FAA Next Gen Nat Clayton, Program Manager 39 th Annual Joseph P. Cribbins Aviation Product Symposium 7 February 2013 Von Braun Center, Huntsville, Alabama
2 Today s Avionics Upgrade Challenge National airspace driven requirements [civilian Interoperability] Improved situational awareness Platform real estate constraints Modernization with bussed avionics Add more functionality within current Size, Weight & Power envelope Achieve all of the above in a shrinking DOD budget 2
3 ASN-128D History The first ASN-128 system was fielded in the early 1980s Since then, the Government and BAE Systems have upgraded the ASN-128 Doppler System to meet the prevailing needs of Army Aviation Upgrade #1: ASN-128A Addition of NVG display to be compatible with night vision goggle (NVG) fielding Upgrade #2: ASN-128B Addition of GPS Receiver, a four-line display, and remove obsolescence Receiver Transmitter Antenna (RTA) Control Display Unit (CDU) Signal Data Converter (SDC) GPS Antenna Upgrade #3: ASN-128C Addition of a Mil-Std-1553B capability (CCA) for MedEvac helicopter Upgrade #4: ASN-128D Addition of a SAASM GPS, IFR certification, and remove obsolescence
4 ASN-128D Current Upgrade Summary PM AME embarking on following ASN-128D upgrades to address FAA NEXTGEN requirements: Improved display capability for critical data with integrated information to decrease Pilot workload Touchscreen Display providing intuitive pilot interface Moving Map Capability USB AMPS data loader capability Vertical Obstruction Overlays Electronic FLIP Charts Flight Planning Steering Hover Indication Display Fuel Calculator Improved flight planning capability GPS as a primary means of navigation (MSO-C145a compliance) ADS-B Out Position Sensor Support External digital video output to drive an external MFD display Mil-Std-1553 Data Bus with Bus Controller capability Dual CDU Configuration capability Triplex Navigation Solution (GPS, Doppler, IMU) Design hooks for future capability (M-Code GPS, JPALS, etc.) Upgrade maintains current system Size, Weight and Power requirements Designed to meet RNP RNAV Requirements Global Air Traffic Management (GATM) Compliant DO-236B, DO-283A, DO-229D SW Functionality and Integrity Enhancement DO-178B, DO-254 Required to meet changes in Civil Navigation Regs P-RNAV, B-RNAV, US RNAV Required to maintain ability to fly in Civil Airspace ADS-B In/Out
5 ASN-128D Roadmap FUTURE UH 60 A/L Software Update CDU Touch Screen Display ASN-128 SW UH-60 A/L SW Upgrade (Primary Means, Mil-Std-1553, ADS-B Out) ASN-128D UH-60 A/L CDU Upgrade (Touch Screen Display, Moving Map, USB AMPS Interface) Integrated Tri-Sensor Navigation Solution ASN-128D UH-60 A/L SDC Upgrade (IMU, Kalman Filter) Altimeter & Displays Upgrade ASN-128D UH-60 A/L RTA Upgrade (Altimetry) Trade Studies reviewed for Future Enhancements Navigation Control Integration Communications Control Integration Identification Control Integration Platform Control Integration ASN-128D UH-60 A/L Navigation Control Head Integration (VOR/ILS, JPALS, BFT, DVE, ADS-B IN) ASN-128D UH-60 A/L Communications Control Head Integration (VOR/ILS, JTRS, AM/FM) ASN-128D UH-60 A/L Identification Control Head Integration ( IFF, Mode-5) ASN-128D UH-60 A/L Platform Control Head Integration (Primary Flight Displays, HUMS, Engine Data) 5
6 Summary of ASN-128D Upgrade Approach ASN-128D upgrade approach is a Modular and Flexible Avionics Architecture Design optimized to provide Future Technology insertions that meet Army Aviators needs, while: Residing within current SWaP constraints Minimizing Platform A-kit impacts Reducing pilot s workload Providing intuitive HMI that minimizes training Integrated System Control Communication JTRS AM/FM Navigation VOR/ILS JPALS BFT DVE Identification CXP Platform HUMS Future Enhancement Functions: M-Code GPS ARAIM VOR/ILS Hardware Solution DME Hardware Solution JPALS Hardware Solution Available Interface Capability Mil-Std-1553B Data Bus ARINC Digital Video Interface (DVI) Ethernet USB Serial (RS-232, RS-422, etc ) Discretes Analogs Enabling the Future while Performing Today
7 Thank you Nat Clayton Program Manager, Rotary Wing Control Systems Communications & Control Systems BAE SYSTEMS 150 Parish Drive, TNJ10100A10 Wayne, NJ Facility: 100 Campus Road, Totowa, NJ 07512, Phone
LYNX MULTILINK SURVEILLANCE SYSTEM
Lynx Brochure 2-18-15_MB-2005-10.qxd 2/20/2015 11:16 AM Page 1 LYNX MULTILINK SURVEILLANCE SYSTEM Aviation Products Lynx Brochure 2-18-15_MB-2005-10.qxd 2/20/2015 11:16 AM Page 2 LYNX NGT-9000 The Lynx
5/4/2016 ht.ttlms.com
Order Template Screen 1 Free Form Lesson Overview 2 Free Form Performance Based CNS Requirements 3 Free Form Performance Based CNS Requirements 4 Single Answer Knowledge Check 5 Free Form Related ICAO
Reliable technology for reliable reference.
SOLID-STATE SYSTEMS VERTICAL REFERENCE SYSTEM - VRS-3000 Go with the system that won t lose momentum. Reliable technology for reliable reference. Accurate flight cues are everything to a pilot. Your flight
SOLID-STATE SYSTEMS VRS / ESIS / EHSI
SOLID-STATE SYSTEMS VRS / ESIS / EHSI VERTICAL REFERENCE SYSTEMS - VRS-3000 & 4000 Go with the system that won t lose momentum Reliable technology for reliable reference. Accurate flight cues are everything
Universal Avionics ERA Barcelona Ross Dickey
Universal Avionics Systems @ ERA Barcelona - 2014 Ross Dickey Universal Product Update UNS Flight Management System EFI-890R and EFI 1040, Electronic Flight Display Systems Attitude & Heading Reference
A Low Cost Modular Approach to Avionics Upgrade and CNS/ATM Compliance for the C-130 Hercules
A Low Cost Modular Approach to Avionics Upgrade and CNS/ATM Compliance for the C-130 Hercules By David Green Innovative Solutions and Support Typical C-130 Display Architecture C-130 EIDS EIDS (Engine
Frequently Asked Questions
Frequently Asked Questions FMS Database Service Web-site Questions 1. Can I change my User Name and Password? 2. Why am I unable to access the FMS Database Service Web-site? 3. When is the new Navigation
GH-3900 ESIS. Aviation Products
GH-3900 ESIS Aviation Products GH-3900 ESIS The GH-3900 Electronic Standby Instrument System (ESIS) represents the next generation of standby technology, taking display and operation flexibility to an
Boeing Communications Strategy
Boeing Communications Strategy Presentation to ATN2004 Rob Mead Date: September 15, 2004 Phone: 253-951-8447 Email: rob.mead@boeing.com Topics Data link in Boeing ATM concepts Boeing communications strategy
MINIMUM EQUIPMENT LIST REGISTRATION: SERIAL #:
23 COMMUNICATIONS 23-1 -05-1 Radio Management Unit (RMU) (Honeywell Equipped Aircraft Only) -10-1 Communications System (VHF & UHF) -10-2 High Frequency (HF) Communication System C 2 1 (O) One may be inoperative
Mercury Mission Systems BuildSAFE Graphics Suite Multicore Software Renderer Scott Engle Director of Business Development
Mercury Mission Systems BuildSAFE Graphics Suite Multicore Software Renderer Scott Engle Director of Business Development Mercury acquires Richland Technologies to compliment MMSI Mercury Mission Systems
TELEMETRY SYSTEMS OF THE FUTURE
TELEMETRY SYSTEMS OF THE FUTURE Item Type text; Proceedings Authors Rauch, William D. Publisher International Foundation for Telemetering Journal International Telemetering Conference Proceedings Rights
Future Roadmap for MEMS Inertial Sensors Used in Aviation Applications
AIRTEC 2013 SENSORS & TESTING (ASAT12) Future Roadmap for Inertial Sensors Used in Aviation Applications 6 th November, 2013 Inertial Sensor Applications Attitude & Heading (AHRS)[$30k] Standby Instrument
RNAV 1 Approval Process
RNAV 1 Approval Process JAA Temporary Guidance Material TGL 10 Published November 2000 P-RNAV meets all PBN requirements for RNAV 1 Operations using DME/DME or GNSS EASA transposing JAA guidance into AMC
Innovation and Excellence in Engineering and Support. Solutions.
Innovation and Excellence in Engineering and Support Marshall Aerospace and Defence Group Airport House The Airport Cambridge CB5 8RX UK T +44 (0) 1223 373737 marshalladg.com Contains public sector information
UAS Operation in National Air Space (NAS) Secure UAS Command and Control
UAS Operation in National Air Space (NAS) Secure UAS Command and Control Dr. Randal Sylvester Division Chief Technologist L3 CSW 26 October 2015 This information consists of L-3 Communications Corporation,
How to reduce the integration time Issues and Potential Solutions. Christophe GINESTET
How to reduce the integration time Issues and Potential Solutions Christophe GINESTET August 29th, 2013 Summary SYSTeam Overview The benefits of virtual integration Gateway between virtual and real integration
MULTIFUNCTION AIRCRAFT FLIGHT SURFACE BETTER AVIONICS VERIFICATION TOOL ELECTRONIC CONTROL UNIT TEST SYSTEM: A. Project Goals
MULTIFUNCTION AIRCRAFT FLIGHT SURFACE ELECTRONIC CONTROL UNIT TEST SYSTEM: A BETTER AVIONICS VERIFICATION TOOL Modern avionics exemplify safety and mission-critical, dependable systems. These systems continue
Merging of Flight Test Data within the UMAT TDS
Merging of Flight Test Data within the UMAT TDS Tjorven Gerhard 1, Tobias Paul 1 1 ESG Elektroniksystem- und Logistik GmbH, Fürstenfeldbruck, Germany tobias.paul@esg.de Abstract: In close cooperation with
SESSION G.1 CONVERGING LIVE AND VIRTUAL ARCHITECTURES FOR TRAINING, TEST AND EVALUATION
SESSION G.1 CONVERGING LIVE AND VIRTUAL ARCHITECTURES FOR TRAINING, TEST AND EVALUATION Common Open Architecture for Test and Training Airborne Instrumentation Packages Presenter: Rob Scott OBJECTIVE Compare
Marshall Aerospace and Defence Group.
Marshall Aerospace and Defence Group. We are a leading independent aerospace and defence company and are respected and trusted worldwide for our expertise in civil, military and commercial aircraft and
SCAlable & ReconfigurabLe Electronics platforms and Tools SCARLETT
SCAlable & ReconfigurabLe Electronics platforms and Tools SCARLETT From the Integrated Modular Avionics the First Generation architecture to the Distributed Modular Electronics solution Page 1 Collaborative
Specifications. Z Microsystems, Inc Summers Ridge Road, San Diego, CA T: F:
Specifications 7X Chassis Size 6.6 H x 17.0 W x 16.4 H Weight 24 lbs (65 lbs with 7 modules, 2 power supplies) PowerPak DC Size 5.85 H x 1.90 W x 11 D Weight 3.4 lbs (each module) 6.8 lbs (redundant pair)
Encoders & Data Acquisition Systems
Teletronics Technology Corporation Total System Solutions Encoders & Data Acquisition Systems TTC designs and manufactures signal conditioning systems, data multiplexing systems and data encoder systems
DoD Siting Clearinghouse
DoD Siting Clearinghouse The Impact of Commercial Renewable Energy Development on Military Systems and National Defense Mission Presented by Mr. David Tancabel Outline Clearinghouse Overview SCH Functional
G1000TM. system overview for the Diamond DA40
G1000TM system overview for the Diamond DA40 Record of Revisions Revision Date of Revision Revision Page Range Description A 02/14/05 2-1 2-15 Initial release. Garmin G1000 System Overview for the DA40
TECHNICAL MANUAL COCKPIT VOICE / FLIGHT DATA RECORDER DOWNLOAD PROCEDURES FOR INTEGRATED VEHICLE HEALTH MANAGEMENT SYSTEM (IVHMS) U.S.
PD 2006-034FDR REV-1 15 April 2008 TECHNICAL MANUAL COCKPIT VOICE / FLIGHT DATA RECORDER DOWNLOAD PROCEDURES FOR INTEGRATED VEHICLE HEALTH MANAGEMENT SYSTEM (IVHMS) U.S. ARMY UH-60A/L P/N K277-0101 (IVHMS
Developing and Testing Networked Avionics Systems and Devices By Troy Troshynski, Avionics Interface Technologies
Developing and Testing Networked Avionics Systems and Devices By Troy Troshynski, Avionics Interface Technologies MIL-STD-1553 The MIL-STD-1553 protocol standard was first published in 1973 by the U.S.
TacNet Tactical Radio (TTR) Overview
TacNet Tactical Radio (TTR) Overview 1 Topics Data Link Solutions Overview Why Small Form Factors Advantages of Small Form Factors Key Performance Characteristics Small Form Factor Interoperability Ease
10.4 HXr EFIS. GRT Avionics. (616) fax (616) above, beyond.
Grand Rapids Technologies, Inc. 10.4 HXr EFIS The large screen EFIS for your experimental airplane. Insets...Preserving the View One look at the HXr and you sense the situational awareness provided by
Zing Test Elite Product Introduction
Zing Test Elite Product Introduction Sept 2010 Agenda Capabilities and Features Comparisons Zing Test Elite Product Overview Zing Ware PC-GBS Overview Manuals and Automated Help Overview Platform Application
Installation Manual. Caution: Preliminary. Due to software development occurring at this time, this manual may contain inaccuracies and omissions.
Installation Manual Caution: Preliminary Due to software development occurring at this time, this manual may contain inaccuracies and omissions. Manual Version: Preliminary Date: 10/18/04 Grand Rapids
SOFTWARE SERVICE BULLETIN NO.: 0740 Rev A
SOFTWARE SERVICE BULLETIN NO.: 0740 Rev A TO: All Garmin Aviation Service Centers DATE: SUBJECT: 400W / 500W Series Unit s software upgrade to Main Software version 3.00 & GPS Software version 3.0 PURPOSE
PITOT / STATIC TESTER
PITOT / STATIC TESTER ADSE 7XX range For all aircrafts Edition 01 (0803121514) PITOT / STATIC TESTER For Laboratory and workshop RVSM Pitot / Static Indicator Replace mercury column ADSE 730 RVSM Pitot
Publications and Training Solutions Course Syllabus:
COURSE TITLE: Gulfstream G280 Pro Line Fusion Level I Operations & Flightline Maintenance EQUIPMENT TYPE: EQUIPMENT NOMENCLATURE PART NUMBER Air Data Computer ADC-3010 822-2083-001 Aircraft Configuration
Load up on the NEW SERIES EL ELECTRONIC LOADS. from Kepco
146-1968 MORE WATTS PER VERTICAL INCH Load up on the NEW SERIES EL ELECTRONIC LOADS from Kepco Model EL 2K-- Single Channel Unit Model EL 1K--100D Dual Channel Unit 1KW - 5KW Modules 4U Height Parallel
ST02992CH FAA Supplemental Type Certificate
ST02992CH FAA Supplemental Type Certificate Installation of Dual Electronic Flight Bag (EFB) System Provisions on Boeing 737 Series Aircraft (FAA STC ST02992CH) OVERVIEW FAA STC ST02992CH. European Aviation
Aviation & Airspace Solutions MODERNIZING SYSTEMS TRANSFORMING OPERATIONS DELIVERING PERFORMANCE
Aviation & Airspace Solutions MODERNIZING SYSTEMS TRANSFORMING OPERATIONS DELIVERING PERFORMANCE Enabling Aircraft Safety With Comprehensive Technology MODERNIZING SYSTEMS TRANSFORMING OPERATIONS DELIVERING
Publications and Training Solutions Course Syllabus:
COURSE TITLE: PROLINE 4 CRJ (200/700/900 series) Level I Operators & Flightline Maintenance EQUIPMENT TYPE: EQUIPMENT NOMENCLATURE PART NUMBER IAPS Card Cage ICC 4004 822 0198 001 IAPS Power Supply PWR
Models HX, HS & WS. Installation Manual
GRT HORIZON Models HX, HS & WS Installation Manual Rev. A February 2009 Grand Rapids Technologies, Inc. 3133 Madison Avenue SE Wyoming MI 49548 616-245-7700 www.grtavionics.com INTENTIONALLY BLANK GRT
MORE WATTS PER VERTICAL INCH. from Kepco
146-1968A MORE WATTS PER VERTICAL INCH Load up on the SERIES EL ELECTRONIC LOADS from Kepco Model EL 2K-- Single Channel Unit Model EL 1K--100D Dual Channel Unit 1KW - 5KW Modules 4U Height Parallel Operation
Load up on the NEW SERIES EL ELECTRONIC LOADS from Kepco
146-1968 MORE WATTS PER VERTICAL INCH Load up on the NEW SERIES EL ELECTRONIC LOADS from Kepco Model EL 2K-200-200 Single Channel Unit Model EL 1K-200-100D Dual Channel Unit 1KW - 5KW Modules 4U Height
Network Object Architectures (NOA) for Avionics Wednesday 20th June 10.00am 1.00pm
www.ruggedfiberoptics.com Network Object Architectures (NOA) for Avionics Wednesday 20th June 10.00am 1.00pm Spring 2018 Aircraft Network Problems Today 1. Complexity Point to point and point to multi-point
ST03006CH FAA Supplemental Type Certificate
ST03006CH FAA Supplemental Type Certificate Installation of a CMC Dual Class 3 Electronic Flight Bag (EFB) System on Boeing 737 Series Aircraft (FAA STC ST03006CH) OVERVIEW FAA STC ST03006CH. European
ST02949CH FAA Supplemental Type Certificate
ST02949CH FAA Supplemental Type Certificate Installation of a Rosemount Aerospace 87600E1 Class 3 Electronic Flight Bag (EFB) System on Boeing 737 Series Aircraft (FAA STC ST02949CH) OVERVIEW FAA STC ST02949CH.
Ferranti Technologies Ltd Rotary & Fixed Wing Solutions
Ferranti Technologies Ltd Rotary & Fixed Wing Solutions Focused on Customers & Driven by Quality Ferranti Technologies Ltd Systems & Solutions Supplier to the world s leading defence organisations, including
MIL-STD-1760 DIGITAL LAUNCHER FOR NAVY/MARINE CORP 2.75-INCH ROCKET SYSTEM. Naval Surface Warfare Center, Indian Head Division
MIL-STD-1760 DIGITAL LAUNCHER FOR NAVY/MARINE CORP 2.75-INCH ROCKET SYSTEM Charles Paras David Culhane Craig Neitzke Naval Surface Warfare Center, Indian Head Division Report Documentation Page Report
MIL-STD-1553 INTERFACES TO TELEMETRY SYSTEMS
MIL-STD-1553 INTERFACES TO TELEMETRY SYSTEMS Ray Nicolais Product Manager Digital Data Systems AYDIN VECTOR Division Newtown, Pennsylvania Donald H. Ellis System Engineer AEROSYSTEMS ASSOCIATES Huntsville,
Vigilant LED Based Obstruction Lights
Vigilant LED Based Obstruction Lights On when it matters most. Products and solutions that protect your business 2 www.dialight.com Obstruction_Brochure_M Features & Benefits 5 year full performance warranty
An Integrated Test Environment for Systems Engineering. Ryan Brooks Roberto Escobar Boeing Mesa, AZ
An Integrated Test Environment for Systems Engineering Ryan Brooks Roberto Escobar Boeing Mesa, AZ 2009 by Boeing; made available under the EPL v1.0 March 25, 2009 What is OSEE s OTE Framework? The Open
Publications and Training Solutions Course Syllabus:
COURSE TITLE: Embraer L500 Pro Line Fusion Level I Operations & Flightline Maintenance EQUIPMENT TYPE: EQUIPMENT NOMENCLATURE PART NUMBER Adaptive Flight Display, 15.1" AFD-6520 822-2332-300 Instrument
Rapid Integration Framework (RIF)
RIF Demonstration Booth Layout Rapid Integration Framework (RIF) Demonstration Information Packet Future Airborne Capability Environment (FACE) Technical Interchange Meeting (TIM) 18 September 2018 Distribution
NEW NETWORK PROTOCOL STANDARD FOR HIGH SPEED CAMERAS
7 th International Symposium on NDT in Aerospace We.3.A.1 More Info at Open Access Database www.ndt.net/?id=18958 NEW NETWORK PROTOCOL STANDARD FOR HIGH SPEED CAMERAS Abstract Reto HUBER 1 1 AOS Technologies
ST02612CH FAA Supplemental Type Certificate
ST02612CH FAA Supplemental Type Certificate Installation of AD Aerospace Cockpit Door Monitoring System on Airbus A318, A319, A320, and A321 Series Aircraft (FAA STC ST02612CH) OVERVIEW FAA STC ST02612CH.
EUROCAE ED-122 / RTCA DO-306 Oceanic SPR Standard
Oceanic SPR Standard ICAO NAT PBCS Workshop, Feb 2013 Presented by Jerome CONDIS RTCA SC-214 / EUROCAE WG-78 Co-chair 1 History SC189 / WG53 1 2 3 4 ED100 / DO 258 : Interoperability Requirements for ATS
Filtering Out of All The Noise
Filtering Out of All The Noise EMI and RFI noise is an elusive and costly problem that may prevent new electronic equipment designs from passing compliance testing. As processing speeds in electronics
Innovation, Quality & Service. MIL-STD-1553 ARINC-429/717 Interface Cards & Real-Time Ethernet Converters.
Innovation, Quality & Service MIL-STD-1553 ARINC-429/717 Interface Cards & Real-Time Ethernet Converters www.altadt.com 1-888-429-1553 Alta Data Technologies Company Overview Founded in 2007, Alta is the
Reaching for the sky with certified and safe solutions for the aerospace market
www.tttech.com/aerospace Reaching for the sky with certified and safe solutions for the aerospace market More about our certified and safe products inside Advancing safe technologies, improving human lives
Page 1 of 13 Report Date: 16-May-2014 OPEN FAULT REPORT
Page 1 of 13 : 11014.7 NO STATUS A 03/05/2012 10:46 am 5 JA015264 10,045.2 #2 ENGINE COWLING HAS II COMPOSITE DAMAGE. ENGINE COWLING RESTRICTED FROM USE AS A WORK PLATFORM IAW H-60-11-ASAM-14 UNTIL REPLACED.
OCS-NG400
Future Ready Voice Communications System OCS-NG400 OCS-NG400 1 www.onur.net 2 OCS-NG400 The OCS-NG400 IP-based voice communications system, combining state-of-the-art technology with proven components
Instrumentation of UAV for 6-DOF Modeling
Instrumentation of UAV for 6-DOF Modeling Quarterly Review of the NASA/FAA Joint University Program for Air Transportation Research Friday June 14 th, 2002 Presented By: Sean M. Calhoun Jacob Campbell
Aerospace Technology Congress 2016 Stockholm, Sweden
SESAR Aerospace Technology Congress 2016 Stockholm, Sweden Michael Standar, SESAR Joint Undertaking 2 ICAO projected global traffic scenario - 2040 The European ATM Master Plan SESAR - addressing global
Chadwick 8500C+ Balancer/Analyzer ONE BALANCER/ANALYZER FOR ALL YOUR NEEDS. Keeps flight time up and maintenance costs down
Chadwick 8500C+ Balancer/Analyzer ONE BALANCER/ANALYZER FOR ALL YOUR NEEDS Keeps flight time up and maintenance costs down The Chadwick 8500C+ comes flight-line ready as a complete kit, with all of the
ATTACHMENT. SB Revision 1 TERRAIN AWARENESS AND WARNING SYSTEM CLASS-B (TAWS-B) ORDER FORM
Single Engine ATTACHMENT TERRAIN AWARENESS AND WARNING SYSTEM CLASS-B (TAWS-B) ORDER FORM The TAWS-B upgrade enhances the current Terrain and Obstacle Proximity Warning System by providing additional integrated
The BOM [Broadcasting Outer Module]
![The BOM [Broadcasting Outer Module]](/thumbs/91/106681333.jpg "The BOM [Broadcasting Outer Module]")
Avionics Reimagined The BOM [Broadcasting Outer Module] The first and only ALL-IN-ONE AVIONICS SUITE Distributed by: Adams Aviation Supply Co Ltd mail@adamsaviation.com www.adamsaviation.com BOM (Broadcasting
roda MilDef Rugged Displays
roda MilDef Rugged Displays Forged in the thick of battle Every roda MilDef RD display was inspired by action in the field. Each design was developed in cooperation with armed forces to meet the ongoing
EUROMED GNSS II/MEDUSA project
EUROMED GNSS II/MEDUSA project PBN Implementation Workshop / Go Team PBN Implementation Workshop / Go Team, Tunis, February 2014 1 Contents Euromed GNSS European GNSS (E GNSS), EGNOS and Galileo Euromed
P L R. Flight Test Data. Recording and Processing. System. March 2000
Flight Test Data Recording and Processing System March 2000 P L R Poleg Industrial Park POB 8130 Netanya 42160 Israel Tel: +972-9-8657670 Fax: +972-9-8657621 Introduction Any flight-testing involves recording
WZRDnet. A Low-Power Wireless Ad-Hoc Mesh Network for Austere Tactical Environments. February 14, 2018
White Paper TELEGRID Technologies, Inc. WZRDnet A Low-Power Wireless Ad-Hoc Mesh Network for Austere Tactical Environments February 14, 2018 23 Vreeland Road Suite 290 Florham Park, NJ 07932 www.telegrid.com
Are you up to the TEST?
Are you up to the TEST? Take the 2012 Technical Training Exam Available online ONLY at: www.aea.net/avionicsnews FAA-accepted training is available to AEA members through the pages of Avionics News. With
! o o o o o o o o o (Per the February 9, 2015 rule change to 14 CFR 91.225 (b)(1)(ii)) (A letter of authorization from the aircraft manufacturer is needed for installation in LSA aircraft) ± ! ADF
TWELFTH AIR NAVIGATION CONFERENCE
International Civil Aviation Organization 7/5/12 WORKING PAPER ANConf.12.WP.007.en.docx TWELFTH AIR NAVIGATION CONFERENCE Montréal, 19 to 30 November 2012 Agenda Item 3: Interoperability and data through
EXPAND YOUR REPROGRAMMING CAPABILITIES. Perform software upgrades and integration tests in-house AN/ARC-210 ANCILLARY TOOLS
WHITE PAPER // JANUARY 2019 AN/ARC-210 ANCILLARY TOOLS EXPAND YOUR REPROGRAMMING CAPABILITIES Perform software upgrades and integration tests in-house INTRODUCTION Collins Aerospace s AN/ARC-210 ancillary
Precision Roadway Feature Mapping Jay A. Farrell, University of California-Riverside James A. Arnold, Department of Transportation
Precision Roadway Feature Mapping Jay A. Farrell, University of California-Riverside James A. Arnold, Department of Transportation February 26, 2013 ESRA Fed. GIS Outline: Big picture: Positioning and
Two-Year Academic Course Schedule - Fall 2017 through Summer Program Director: Eric Himler Campus Phone :
AVT 101 Private Pilot Ground School 4.00 GR M GR M GR M GR M AVT 102 Private Pilot Flight 4.00 O ARR O ARR O ARR O ARR AVT 103 Intro to ATC 3.00 GR M GR M GR M GR M AVT 105 Aviation Meteorology 4.00 GR
Mounted Family of Computer Systems (MFoCS)
Mounted Family of Computer Systems (MFoCS) MOUNTED FAMILY OF COMPUTER SYSTEMS (MFoCS) TODAY S GENERATION OF WARFIGHTER DESERVES A NEXT-GENERATION MOUNTED COMPUTER. MFoCS improves Situational Awareness
Publications and Training Solutions Course Syllabus:
COURSE TITLE: Pro Line Fusion King Air C90GT/B200Gt/B200CGT/B300 Level I Operations & Flight Line Maintenance PREREQUISITES: Students should have basic knowledge of aircraft avionics systems and a working
EASA Proposed CM-AS-002 Issue 01 Clarifications to AMC Comment Response Document
Proposed CM-AS-002 Issue 01 Clarifications to AMC 20-27 - Response Document summary Suggested resolution is is 1 Cessna Aircraft Compy --- --- Cessna Aircraft Compy has no on this issue at this time. Noted
SG102 AHRS. See what s next
SG102 AHRS The Sandel SG102 (MOD2) Attitude Heading Reference System (AHRS) has an initialization time that is 3Xs faster then the previous version. It also now comes with selectable low- and high-speed
2U/5U. AC + DC Power Solutions. Transient Generation for Disturbance Tests. only. High Performance Programmable AC Power Source
AFV-P series High Performance Programmable AC Power Source only 2U/5U i Output Frequency up to 15-1000Hz Intuitive Touch Screen HMI AC Source with DC output AC & DC Transient Generation for Disturbance
National Instruments Approach
National Instruments Approach Our graphical programming software, LabVIEW, and modular, open hardware, has redefined how engineers work throughout the entire product design cycle. Committed to Engineers
APP - Aircraft Performance Program
Introduction APP - Aircraft Performance Program Introduction APP is an aircraft-performance calculation program, specifically designed to provide a fast and easy way to evaluate aircraft performance. Another
NTPS Aeronautical Mobile Telemetry Technology Upgrade. 11-May-2017 Stephanie Luongo, National Test Pilot School Paul Chamberlain, Nginuity
NTPS Aeronautical Mobile Telemetry Technology Upgrade 11-May-2017 Stephanie Luongo, National Test Pilot School Paul Chamberlain, Nginuity 1 Outline Background C/L Band Datalink Upgrades ~ Key Driving Requirements
SDR MAINTENANCE INTERFACE PANEL
SDR MAINTENANCE INTERFACE PANEL USER'S MANUAL (version 3.0) www.db-integrations.com Table Of Contents: Maintenance Panel Overview:...4 User's Manual Applicability:...4 Equipment Part Numbers:...4 Physical
BIGGER. BETTER. BOLDER. SAFECRAFT. A portfolio of safety-related equipment
BIGGER. BETTER. BOLDER. SAFECRAFT A portfolio of safety-related equipment StandardAero SAFECRAFT A portfolio of safety technologies focused on incident prevention Operators are able to select items from
ARINC 818. Avionics Digital Video Bus. Development Suite
ARINC 818 Avionics Digital Video Bus Development Suite ARINC 818 Development Suite Great River offers a complete set of tools to support your ARINC 818 project. Already, Great River s ARINC 818 tools have
HMI Heavy - Duty Series HDS-4
INDUSTRIAL PANEL PC S Human Machine Interface (HMI) Heavy - Duty Series From general purpose computing to highly customized applications PRIMARY NETWORKS has a solution. Our HMIs are designed for severe
Open Standards in Aircraft Instrumentation
Open Standards in Aircraft Instrumentation Robert Hill Eglin AFB, FL 96 th Test Wing 96 th Range Group 896 th Test Support Squadron Outline Background Challenges Why Standards? What Standards are Needed?
ForneyLink TM Touchscreen User Interface
ForneyLink TM Touchscreen User Interface Digital Readout with Full Data Acquisition Digital Readout ForneyLink TM is an intuitive, comprehensive, digital display of significant, relevant material testing
Standardizing Warfare System Interfaces to Reduce Integration Costs During Ship Construction, Modernization, and Maintenance
Standardizing Warfare System Interfaces to Reduce Integration Costs During Ship Construction, Modernization, and Maintenance F. Scott Parks 15 March 2016 Study Guidance Objectives Identify commercial data
ROTARY WING AVIONICS COMPONENT SOLUTIONS
RTARY IN AVINICS CMPNENT SLUTINS CUNT N CLLINS FR PRVEN RTARY IN PERFRMANCE Rockwell Collins has a full-range of proven rotary wing avionics solutions available. ur complete selection of rotary wing equipment
Installation of DynaFlight-III System
DynaNav Systems Inc. 730 11731 Baynes Road Pitt Meadows. BC, Canada, V3Y 2B3 www.dynanav.com THIS MANUAL CONTAINS HELPFUL HINTS ON: Installation of DynaFlight-III System DynaFlight Airborne Aerial Application
J.P.Instruments Inc B Airway Ave Costa Mesa CA Fax
Date 4-8-2014 Page 1 of 6 J.P.Instruments Inc.. 3185B Airway Ave Costa Mesa CA 92626 714 557 3805 Fax 714 557 9840 EDM 960 Instructions for Continued Airworthiness Supplement No: 960-01 Revision: IR Prepared
Military Data Link Integration Application James T. Sturdy
Military Data Link Integration Application James T. Sturdy Honeywell Defense and Space Electronic Systems 9201 San Mateo Blvd., NE Albuquerque, New Mexico 87113-2227 (505) 828-5703 Office (505) 828-5500
U.S. Department of Transportation. Standard
U.S Department of Transportation Federal Aviation Administration U.S. Department of Transportation Federal Aviation Administration Standard DATA STANDARD FOR THE NATIONAL AIRSPACE SYSTEM (NAS) Foreword
SERVICE BULLETIN. 525A (CJ2+) thru -0416, thru -0438
TITLE SB NAVIGATION - COLLINS IFIS 6.0 SYSTEM SOFTWARE UPDATES EFFECTIVITY MODEL SERIAL NUMBERS 525A (CJ2+) -0300 thru -0416, -0418 thru -0438 REASON The equivalent of this service bulletin has been incorporated
Inertial Systems. Ekinox Series TACTICAL GRADE MEMS. Motion Sensing & Navigation IMU AHRS MRU INS VG
Ekinox Series TACTICAL GRADE MEMS Inertial Systems IMU AHRS MRU INS VG ITAR Free 0.05 RMS Motion Sensing & Navigation AEROSPACE GROUND MARINE Ekinox Series R&D specialists usually compromise between high
EE4001: Final Year Project Continuous Assessment 1
EE4001: Final Year Project Continuous Assessment 1 Universal Control Methodology Design and Implementation for Unmanned Vehicles Phang Swee King 24 th September 2009 Outlines Introduction Goal of the Project
Microair Avionics Pty Ltd Airport Drive Bundaberg Queensland 4670 Australia Tel: Fax:
Microair Avionics Pty Ltd Airport Drive Bundaberg Queensland 4670 Australia Tel: +61 7 41 553048 Fax: +61 7 41 553049 e-mail: support@microair.com.au About This Document This manual describes the various
Dynamic Power Management in the Data Center
Dynamic Power Management in the Data Center IBM Power and Cooling Symposium Raleigh, NC 04 October 2007 Bharat S. Shah Emerson Network Power Bharat.Shah@EmersonNetworkPower.com Agenda Power Management