AADL Fault Modeling and Analysis Within an ARP4761 Safety Assessment
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A Zonal Safety Analysis Methodology for Preliminary Aircraft Systems and Structural Design
A Zonal Safety Analysis Methodology for Preliminary Aircraft Systems and Structural Design Chen, Z. and Fielding, J. P. School of Aerospace, Transport and Manufacturing, Cranfield University ABSTRACT Zonal Safety Analysis (ZSA) is a major part of the civil aircraft safety assessment process described in Aerospace Recommended Practice 4761 (ARP4761). It considers safety effects that systems/items installed in the same zone (i.e. a defined area within the aircraft body) may have on each other. Although the ZSA may be conducted at any design stage, it would be most cost-effective to do it during preliminary design, due to the greater opportunity for influence on system and structural designs and architecture. The existing ZSA methodology of ARP4761 was analysed but it was found to be more suitable for detail design rather than preliminary design. The authors therefore developed a methodology that would be more suitable for preliminary design and named it the Preliminary Zonal Safety Analysis (PZSA). This new methodology was verified by means of the use of a case-study, based on the NASA N3-X project. Several lessons were learnt from the case study, leading to refinement of the proposed method. These lessons included focusing on the positional layout of major components for the zonal safety inspection, and using the Functional Hazard Analysis (FHA)/Fault Tree Analysis (FTA) to identify system external failure modes. The resulting PZSA needs further refinement, but should prove to be a useful design tool for the preliminary design process. _____________________________________ INTRODUCTION This paper outlines the development of a methodology, hereafter referred to as the Preliminary Zonal Safety Historically, system safety analysis was primarily based Analysis (PZSA). -
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NASA/CR–2015-218982 Application of SAE ARP4754A to Flight Critical Systems Eric M. Peterson Electron International II, Inc., Phoenix, Arizona November 2015 NASA STI Program . in Profile Since its founding, NASA has been dedicated to the CONFERENCE PUBLICATION. advancement of aeronautics and space science. The Collected papers from scientific and technical NASA scientific and technical information (STI) conferences, symposia, seminars, or other program plays a key part in helping NASA maintain meetings sponsored or this important role. co-sponsored by NASA. The NASA STI program operates under the auspices SPECIAL PUBLICATION. Scientific, of the Agency Chief Information Officer. It collects, technical, or historical information from NASA organizes, provides for archiving, and disseminates programs, projects, and missions, often NASA’s STI. The NASA STI program provides access concerned with subjects having substantial to the NTRS Registered and its public interface, the public interest. NASA Technical Reports Server, thus providing one of the largest collections of aeronautical and space TECHNICAL TRANSLATION. science STI in the world. Results are published in both English-language translations of foreign non-NASA channels and by NASA in the NASA STI scientific and technical material pertinent to Report Series, which includes the following report NASA’s mission. types: Specialized services also include organizing TECHNICAL PUBLICATION. Reports of and publishing research results, distributing completed research or a major significant phase of specialized research announcements and feeds, research that present the results of NASA providing information desk and personal search Programs and include extensive data or theoretical support, and enabling data exchange services. analysis. Includes compilations of significant scientific and technical data and information For more information about the NASA STI program, deemed to be of continuing reference value. -
Quality Assurance, Process Engineer
THOMMEN AIRCRAFT EQUIPMENT Renowned Swiss manufacturer of high precision Aviation Instruments, Air Data Computers, Digital Chronometers and Mission Equipment Established in 1853 under Revue Thommen AG, Thommen Aircraft Equipment Ltd is a renowned Swiss manufacturer of high precision aviation instruments, avionics and mission equipment. The company has celebrated its 100 years anniversary of supplying aviation products to its customers. Thommen Aircraft Equipment AG is currently in the phase of introducing several innovative and exciting products to the market and will gradually increase the general product offering in the course of 2018/2019. To sustain the new company plans, product development, we are looking to hire a skilled and experienced Quality Assurance / Process Engineer – Avionics 100% (m/f) The person will be responsible for leading activities involving Product Lifecycle Management processes. Focused on improving processes and tools, the position is ideal for a candidate seeking a broad technical and business process career. The position offers the opportunity to work as part of a global team which will require flexibility to support activities across multiple time zones for following process development activities. Our culture is to hire only the finest talent and to uphold our values of teamwork, accountability, humor, efficiency, candor and continual improvement. Responsibilities & Tasks • Develop DO-178C and DO-254 process compliance and quality plan, (QAP, SQAP HQAP) • Responsible for reporting assessment and evaluation -
SAE International® PROGRESS in TECHNOLOGY SERIES Downloaded from SAE International by Eric Anderson, Thursday, September 10, 2015
Downloaded from SAE International by Eric Anderson, Thursday, September 10, 2015 Connectivity and the Mobility Industry Edited by Dr. Andrew Brown, Jr. SAE International® PROGRESS IN TECHNOLOGY SERIES Downloaded from SAE International by Eric Anderson, Thursday, September 10, 2015 Connectivity and the Mobility Industry Downloaded from SAE International by Eric Anderson, Thursday, September 10, 2015 Other SAE books of interest: Green Technologies and the Mobility Industry By Dr. Andrew Brown, Jr. (Product Code: PT-146) Active Safety and the Mobility Industry By Dr. Andrew Brown, Jr. (Product Code: PT-147) Automotive 2030 – North America By Bruce Morey (Product Code: T-127) Multiplexed Networks for Embedded Systems By Dominique Paret (Product Code: R-385) For more information or to order a book, contact SAE International at 400 Commonwealth Drive, Warrendale, PA 15096-0001, USA phone 877-606-7323 (U.S. and Canada) or 724-776-4970 (outside U.S. and Canada); fax 724-776-0790; e-mail [email protected]; website http://store.sae.org. Downloaded from SAE International by Eric Anderson, Thursday, September 10, 2015 Connectivity and the Mobility Industry By Dr. Andrew Brown, Jr. Warrendale, Pennsylvania, USA Copyright © 2011 SAE International. eISBN: 978-0-7680-7461-1 Downloaded from SAE International by Eric Anderson, Thursday, September 10, 2015 400 Commonwealth Drive Warrendale, PA 15096-0001 USA E-mail: [email protected] Phone: 877-606-7323 (inside USA and Canada) 724-776-4970 (outside USA) Fax: 724-776-0790 Copyright © 2011 SAE International. All rights reserved. No part of this publication may be reproduced, stored in a retrieval system, distributed, or transmitted, in any form or by any means without the prior written permission of SAE. -
Risk Assesment: Fault Tree Analysis
RISK ASSESMENT: FAULT TREE ANALYSIS Afzal Ahmed+, Saghir Mehdi Rizvi*Zeshan Anwer Rana* Faheem Abbas* +COMSAT Institute of Information and Technology, Sahiwal, Pakistan *Navy Engineering College National University of Sciences and Technology, Islamabad drafzal@ciitsahiwal>edu.pk, 03452325972 ABSTRACT The failure of engineering equipment causes loss of capital as well as human loss, injuries, and stoppage of production line. The hazards can be classified as safe, minor, major, critical and catastrophic Risk analysis or hazard analysis pin points the potential failures of engineering systems and or components when being used.. Failure mode and effects analysis is used to identify hazard and to make system safer. A system is broken down up to level of components and using reliability data the safety or probability of failure of assemblies and the system can be calculated. The failure mode and effects analysis is used with fault tree analysis to point the areas of a complex system where failure mode effect analysis is required. Fault tree analysis (FTA) is a technique which pinpoints any failure or severe accidents. It tells how things fail rather than emphasize on the design performance. It is a logic diagram connecting inputs an outputs using Boolean algebra. This paper shows how FTA can be applied to car carburetor failure and car brake failure. Key words : Risk Management, Reliability, Fault tree, Failure mode INTRODUCTION The world is full risk. We are at risk of accident minor. A failure of an aircraft may cause death when crossing a road or driving. We are at risk to passengers, while a machine may cause living in an apartment not properly designed. -
Learn More About the GM Foundation's
“I joined SAE as a student member when SAE INTERNATIONAL I was an 18-year-old AND GM FOSTER college freshman, and now, as an SAE THE ENGINEERS OF Foundation Trustee for TOMORROW fi ve years, I’m inspired and honored to be giving back. We want to help young people General Motors and SAE International have teamed up to provide of all ages understand K–college students with stimulating, hands-on STEM educational opportunities guided by industry experts. These programs aim to inspire how great engineering curiosity in STEM education and ultimately transform today’s students into careers are and help tomorrow’s engineers. By supporting the SAE Foundation, the charitable them prepare for those arm of SAE, General Motors aligns its business needs with an organization dedicated to the development of the future workforce. careers. We envision a future with more Fueled by GM’s contributions, beginning in 1986, including a $5 million gift engineers—because we in 2004 and almost $2 million since, these two organizations have been believe it will make the making unparalleled impact in STEM curriculum development and delivery, reaching hundreds of thousands of students, and providing GM employees world a better place.” with inspiring and engaging volunteer opportunities through SAE’s STEM — Dan Nicholson, Vice President education programs. Over the years, GM has fully funded initiatives of Electrifi cation, Controls, Software & Electronic Hardware including Fuel Cell Challenge, Gravity Cruiser, Making Music Challenge and the soon-to-be-released Programming Each Other. GM’s employee volunteers serve as formal mentors and volunteers throughout the academic year, and the number of participants continues to trend upward, increasing from 1,463 in 2014 to 1,826 in 2017. -
Visit of Dan Hancock, SAE Intl. President
August 2014 A Newsletter from Visit of Dan Hancock, SAE Intl. President AWIM- Jet toy demonstration by school children COLT Hyderabad KRT launch at Mahindra Research Valley And more inside… August 2014 Lap NO: SAEISS/14/02 August 2014 Chairman’s Message…4 Contents Professional members Space…… 5 5 7 Lecture KRT meeting launch 10 Top Tech Student members Space..... 13 13 14 Student’s COLT Hyderabad convention 15 17 SAE Trek AWIM 2 August 2014 About … SAEINDIA Southern Section is a premier society that serves the cause of mobility engineering. It is a unique society that includes professional engineers who serve different OEMS and Suppliers, academia as well as budding engineers (students) who aspire to be part of the professionally attractive field of mobility engineers. We believe that Mobility Engineering is a knowledge rich field and that learning and sharing can be fun and rewarding. To this end, SAEISS organizes several events throughout the year, runs programmes that enrich and engage and conducts lectures and symposia. It is a part of SAEINDIA. SAEINDIA is an affiliate society of SAE International which is head quartered in USA and has a glorious record of over 100 years of service to the mobility community. This newsletter is brought for Information Cascading among SAEINDIA members Editorial Team: Patron: Balasubramanian N Editor : Mr. Vijayaragavan N- RNTBCI SAEISS office: M/s,Hari prasan dash , S. Ilangovan, Mukesh, Panneerselvam, Vasanth Raj Industry members: M/s Padmesh sewda (RNTBCI), Vinothkumar B (RNTBCI), Sivashankar S (RNTBCI), Sanjeev Bhushan (Daimler), Venkatesan (Royal Enfield), Sreevalsan (UCAL fuel) Student executive council members (SEC):, M/s Shankara narayanan P, Pulkit goel, Venkata raghav , Md. -
SAE COLLEGIATE DESIGN SERIES 2015 Season Recap
MOMENTUM TM THE MAGAZINE FOR STUDENT MEMBERS OF SAE INTERNATIONAL SAE COLLEGIATE DESIGN SERIES 2015 season recap BEST BOOTH University of Puerto Rico–Mayaguez team wins Student Exhibit Competition Stemming the STEM crisis Getting through to kids early CONTENTS 2 EDITORIAL STEM REPORT FEATURE 3 BRIEFS 14 Taking action early to conquer the Vol 6 STEM crisis Issue 4 STUDENT GENERATION Interest in STEM subjects falls precipitously as students progress through elementary and middle school. FEATURE 4 UMich-Ann Arbor team takes home Baja season’s Iron Team Award TODAY’S ENGINEERING Cornell University also had a strong 2014 season, but not 16 Energid actively working on strong enough to fend off Michigan Baja Racing. simulation technologies for lunar and planetary rovers FEATURE 6 Georgia Tech and Warsaw University were double-winners at SAE Aero 17 Blizzard conditions test FCA’s 4WD Design competitions and AWD vehicles University of Akron and University of Cincinnati were the other winners at the twin 3-class competitions, the SAE NETWORKING former setting a record in the process. 18 Unstoppable Formula SAE team leader earns Rumbaugh Award FEATURE 8 West Coast teams win 2 of 3 Formula 19 Give a presentation at the SAE 2016 SAE events World Congress Oregon State captures its fifth crown while San Jose State enjoys its first overall victory and UPenn tops the electric 19 Doug Gore remembered for SAE field. volunteerism 10 UW-Madison tops IC engine field at SAE Clean Snowmobile Challenge 20 GEAR 11 Université Laval repeats as SAE 11 Supermileage champ 12 Team from the University of Waterloo ON THE COVER CARS ARE LINED UP AND READY TO ROAR AT THE BAJA SAE sets record in winning Formula Hybrid AUBURN EVENT. -
NASA Fault Tree Handbook with Aerospace Applications
Fault Tree Handbook with Aerospace Applications Version 1.1 FFFaaauuulllttt TTTrrreeeeee HHHaaannndddbbbooooookkk wwwiiittthhh AAAeeerrrooossspppaaaccceee AAAppppppllliiicccaaatttiiiooonnnsss Prepared for NASA Office of Safety and Mission Assurance NASA Headquarters Washington, DC 20546 August, 2002 Fault Tree Handbook with Aerospace Applications Version 1.1 FFFaaauuulllttt TTTrrreeeeee HHHaaannndddbbbooooookkk wwwiiittthhh AAAeeerrrooossspppaaaccceee AAAppppppllliiicccaaatttiiiooonnnsss NASA Project Coordinators: Dr. Michael Stamatelatos, NASA Headquarters Office of Safety and Mission Assurance Mr. José Caraballo, NASA Langley Research Center Authors: NASA Dr. Michael Stamatelatos, NASA HQ, OSMA Lead Author: Dr. William Vesely, SAIC Contributing Authors (listed in alphabetic order): Dr. Joanne Dugan, University of Virginia Mr. Joseph Fragola, SAIC Mr. Joseph Minarick III, SAIC Mr. Jan Railsback, NASA JSC Fault Tree Handbook with Aerospace Applications Version 1.1 FFFaaauuulllttt TTTrrreeeeee HHHaaannndddbbbooooookkk wwwiiittthhh AAAeeerrrooossspppaaaccceee AAAppppppllliiicccaaatttiiiooonnnsss Acknowledgements The project coordinators and the authors express their gratitude to NASA Office of Safety and Mission Assurance (OSMA) management (Dr. Michael Greenfield, Deputy Associate Administrator and Dr. Peter Rutledge, Director of Enterprise Safety and Mission Assurance) and to Mr. Frederick Gregory, NASA Deputy Administrator, for their support and encouragement in developing this document. The authors also owe thanks to a number of reviewers -
Hazard Analysis of Complex Spacecraft Using Systems- Theoretic Process Analysis *
Hazard Analysis of Complex Spacecraft using Systems- Theoretic Process Analysis * Takuto Ishimatsu†, Nancy G. Leveson‡, John P. Thomas§, and Cody H. Fleming¶ Massachusetts Institute of Technology, Cambridge, Massachusetts 02139 Masafumi Katahira#, Yuko Miyamoto**, and Ryo Ujiie†† Japan Aerospace Exploration Agency, Tsukuba, Ibaraki 305-8505, Japan Haruka Nakao‡‡ and Nobuyuki Hoshino§§ Japan Manned Space Systems Corporation, Tsuchiura, Ibaraki 300-0033, Japan Abstract A new hazard analysis technique, called System-Theoretic Process Analysis, is capable of identifying potential hazardous design flaws, including software and system design errors and unsafe interactions among multiple system components. Detailed procedures for performing the hazard analysis were developed and the feasibility and utility of using it on complex systems was demonstrated by applying it to the Japanese Aerospace Exploration Agency H-II Transfer Vehicle. In a comparison of the results of this new hazard analysis technique to those of the standard fault tree analysis used in the design and certification of the H-II Transfer Vehicle, System-Theoretic Hazard Analysis found all the hazardous scenarios identified in the fault tree analysis as well as additional causal factors that had not been) identified by fault tree analysis. I. Introduction Spacecraft losses are increasing stemming from subtle and complex interactions among system components. The loss of the Mars Polar Lander is an example [1]. The problems arise primarily because the growing use of software allows engineers to build systems with a level of complexity that precludes exhaustive testing and thus assurance of the removal of all design errors prior to operational use [2,3] Fault Tree Analysis (FTA) and Failure Modes and Effects Analysis (FMEA) were created long ago to analyze primarily electro-mechanical systems and identify potential losses due to component failure. -
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APRIL 9-11 2019 DETROIT TM DOWNLOAD EVENT GUIDE OUR EVENT APP sae.org/wcx Sponsored by Honda In Partnership with 2 WCX THANK YOU TO THE FOLLOWING COMPANIES FOR THEIR GENEROUS SUPPORT. WCX 1 EMERGENCY PROCEDURES DURING WCX CONTENTS During the event attendees are to follow the established emergency guidelines of the facility where the emergency occurs. Based on the Sponsors 1 location of the incident, report emergencies to the nearest venue representative and/or security personnel if available, or report to Information 4 the SAE registration area. Should a catastrophic event occur, attendees should follow the safety Special Events 8 and security instructions issued by the facility at the time of the event. This includes listening for instructions provided through the public Floor Plan 16 address system and following posted evacuation routes if required. Technical Sessions 30 In the event of an emergency or a major disruption to the schedule of events at the event, attendees and exhibitors may call this number Exhibitor Directory 37 to receive further information about the resumption of this event. Updates will also be provided via the SAE website at sae.org. Ad Index Inside Back Cover SAE EMERGENCY HOTLINE +1.800.581.9295 Customer Service +1.877.606.7323 WCX LEADERSHIP TEAM FIRST AID SERVICES C1 Ray Corbin Tuesday, April 9 Taylor Frey AVL 7:00 a.m.–5:00 p.m. Doug Patton Wednesday, April 10 DENSO International America, Inc. 7:00 a.m.–5:00 p.m. Joe Guertin Thursday, April 11 FCA US LLC 7:00 a.m.–8:00 p.m. -
Safety Assessment Processes of ARP4761: Major Revision
Safety Assessment Processes of ARP4761: Major Revision Jim Marko Manager, Aircraft Integration & Safety Assessment 14 November 2018 Presentation Outline • What is changing • ARP4761 Relationship to ARP4754A Development Assurance • New methods • Changes to existing methods • Safety methods other than ARP4761A 14 November 2018 2 ARP4761A Safety Assessment Process What’s happening to ARP 4761? • Revision commenced in early 2012 within the SAE S18 Aircraft & Systems Development and Safety Assessment Committee. • Essentially a near complete revision of the document that is nearing publication. • New processes and analytical methods being added to reflect the trend towards more highly integrated and increasingly complex system designs. • Introduces the concept of Aircraft-Level safety assessment to complement the traditional system-level safety assessment approach. 14 November 2018 3 Current ARP 4761 Rev- New Appendices for ARP 4761 Other Appendices Rev A Developments Functional Hazard Aircraft Functional Hazard Assessment Single Event Effects Assessment AIR 6218 Preliminary System Safety Preliminary Aircraft Safety Assessment Assessment System Functional Hazard Assessment In-Service Safety System Safety Assessment Aircraft Safety Assessment Assessment ARP 5150/5151 FTA, DD, FMEA, Markov Cascading Effects Analysis Common Mode Analysis Development Assurance Assignment Particular Risk Analysis Model Based Safety Assessment Zonal Safety Analysis Contiguous Example Contiguous Example 14 November 2018 4 ARP4761A Safety Assessment Process Interactions ARP 4754A Development Assurance Processes 14 November 2018 5 ARP4761 Relationship to ARP4754A Development Assurance • Modern aircraft architecture is increasingly becoming a “system-of-systems”, where many systems interact with and are dependent upon each other to perform aircraft functional objectives. • The era of having federated systems that can be correctly and completely assessed in silos, independent from other systems, is rapidly closing.