Reengineering Systems Engineering Joseph Kasser, National University of Singapore; Derek Hitchins, ASTEM, Consultant Systems Architect; Thomas V
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Capabilities in Systems Engineering: an Overview
Capabilities in Systems Engineering: An Overview Gon¸caloAntunes and Jos´eBorbinha INESC-ID, Rua Alves Redol, 9 1000-029 Lisboa Portugal {goncalo.antunes,jlb}@ist.utl.pt, WWW home page: http://web.ist.utl.pt/goncalo.antunes Abstract. The concept of capability has been deemed relevant over the years, which can be attested by its adoption in varied domains. It is an abstract concept, but simple to understand by business stakeholders and yet capable of making the bridge to technical aspects. Capabilities seem to bear similarities with services, namely their low coupling and high cohesion. However, the concepts are different since the concept of service seems to rest between that of capability and those directly related to the implementation. Nonetheless, the articulation of the concept of ca- pability with the concept of service can be used to promote business/IT alignment, since both concepts can be used to bridge different concep- tual layers of an enterprise architecture. This work offers an overview of the different uses of this concept, its usefulness, and its relation to the concept of service. Key words: capability, service, alignment, information systems, sys- tems engineering, strategic management, economics 1 Introduction The concept of capability can be defined as \the quality or state of being capable" [19] or \the power or ability to do something" [39]. Although simple, it is a powerful concept, as it can be used to provide an abstract, high-level view of a product, system, or even organizations, offering new ways of dealing with complexity. As such, it has been widely adopted in many areas. -
Need Means Analysis
The Systems Engineering Tool Box Dr Stuart Burge “Give us the tools and we will finish the job” Winston Churchill Needs Means Analysis (NMA) What is it and what does it do? Needs Means Analysis (NMA) is a systems thinking tool aimed at exploring alternative system solutions at different levels in order to help define the boundary of the system of interest. It is based around identifying the “need” that a system satisfies and using this to investigate alternative solutions at levels higher, the same and lower than the system of interest. Why do it? At any point in time there is usually a “current” or “preferred” solution to a particular problem. In consequence organizations will develop their operations and infrastructure to support and optimise that solution. This preferred solution is known as the Meta-Solution. For example Toyota, Ford, General Motors, Volkswagen et al all have the same meta-solution when it comes to automobile – in simple terms two-boxes with wheel at each corner. All of the automotive companies have slowly evolved in to an industry aimed at optimising this meta-solution. Systems Thinking encourages us to “step back” from the solution to consider the underlying problem or purpose. In the case of an automobile, the purpose is to “transport passengers and their baggage from one point to another” This is also the purpose of a civil aircraft, passenger train and bicycle! In other words for a given purpose there are alternative meta-solutions. The idea of a pre-eminent meta-solution has also been discussed by Pugh (1991) who introduced the idea of dynamic and static design concepts. -
Putting Systems to Work
i PUTTING SYSTEMS TO WORK Derek K. Hitchins Professor ii iii To my beloved wife, without whom ... very little. iv v Contents About the Book ........................................................................xi Part A—Foundation and Theory Chapter 1—Understanding Systems.......................................... 3 An Introduction to Systems.................................................... 3 Gestalt and Gestalten............................................................. 6 Hard and Soft, Open and Closed ............................................. 6 Emergence and Hierarchy ..................................................... 10 Cybernetics ........................................................................... 11 Machine Age versus Systems Age .......................................... 13 Present Limitations in Systems Engineering Methods............ 14 Enquiring Systems................................................................ 18 Chaos.................................................................................... 23 Chaos and Self-organized Criticality...................................... 24 Conclusion............................................................................ 26 Chapter 2—The Human Element in Systems ......................... 27 Human ‘Design’..................................................................... 27 Human Predictability ........................................................... 29 Personality ............................................................................ 31 Social -
Launch Options for the Future: a Buyer's Guide (Part 7 Of
— Chapter 3 Enhanced Baseline CONTENTS , Page Improving the Shuttle . 27 Advanced Solid Rocket Motors (ASRMs) . 27 Liquid Rocket Boosters (LRBs) . 28 Lighter Tanks . 29 Improving Shuttle Ground Operations . 29 Improving Existing ELVs . 29 Delta . 30 Atlas-Centaur . ● ● . .* . 30 Titan . ● . ✎ ✎ . 30 Capability . ✎ . ✎ ✎ . ● ✎ ✎ . 30 Table 3-1. Theoretical Lift Capability of Enhanced U.S. Launch Systems. 31 Chapter 3 Enhanced Baseline The ENHANCED BASELINE option is the U.S. Government’s “Best Buy” if . it desires a space program with current or slightly greater levels of activity. By making in- cremental improvements to existing launch vehicles, production and launch facilities, the U.S. could increase its launch capacity to about 1.4 million pounds per year to LEO. The investment required would be low compared to building new vehicles; however, the ade- quacy of the resulting fleet resiliency and dependability is uncertain. This option would not provide the low launch costs (e.g. 10 percent of current costs) sought for SDI deploy- ment or an aggressive civilian space initiative, like a piloted mission to Mars, IMPROVING THE SHUTTLE The Shuttle, though a remarkable tech- . reducing the number of factory joints and nological achievement, never achieved its in- the number of parts, tended payload capacity and recent safety . designing the ASRMs so that the Space modifications have further degraded its per- Shuttle Main Engines no longer need to formance by approximately 4,800 pounds. be throttled during the region of maxi- Advanced Solid Rocket Motors (ASRMs) or mum dynamic pressure, Liquid Rocket Boosters (LRBs) have the potential to restore some of this perfor- ● replacing asbestos-bearing materials, mance; studies on both are underway. -
Fundamentals of Systems Engineering
Fundamentals of Systems Engineering Prof. Olivier L. de Weck Session 12 Future of Systems Engineering 1 2 Status quo approach for managing complexity in SE MIL-STD-499A (1969) systems engineering SWaP used as a proxy metric for cost, and dis- System decomposed process: as employed today Conventional V&V techniques incentivizes abstraction based on arbitrary do not scale to highly complex in design cleavage lines . or adaptable systems–with large or infinite numbers of possible states/configurations Re-Design Cost System Functional System Verification Optimization Specification Layout & Validation SWaP Subsystem Subsystem . Resulting Optimization Design Testing architectures are fragile point designs SWaP Component Component Optimization Power Data & Control Thermal Mgmt . Design Testing . and detailed design Unmodeled and undesired occurs within these interactions lead to emergent functional stovepipes behaviors during integration SWaP = Size, Weight, and Power Desirable interactions (data, power, forces & torques) V&V = Verification & Validation Undesirable interactions (thermal, vibrations, EMI) 3 Change Request Generation Patterns Change Requests Written per Month Discovered new change “ ” 1500 pattern: late ripple system integration and test 1200 bug [Eckert, Clarkson 2004] fixes 900 subsystem Number Written Number Written design 600 major milestones or management changes component design 300 0 1 5 9 77 81 85 89 93 73 17 21 25 29 33 37 41 45 49 53 57 61 65 69 13 Month © Olivier de Weck, December 2015, 4 Historical schedule trends -
ミルスペース 140710------[What’S New in Virtual Library?]
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -ミルスペース 140710- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - [What’s New in Virtual Library?] AW&ST Aviation Week & Space Technology 1406F_Contents.pdf, Cover.jpg 140630AWST_Contents.pdf, Cover.jpg 1405F_Contents.pdf, Cover.jpg NASA Spaceport Magazine 1404F_Contents.pdf, Cover.jpg 1407ksc_Spaceport_Mag_27pages.pdf 1403F_Contents.pdf, Cover.jpg 1407ksc_Spaceport_Mag_Contents.pdf, Cover.jpg Military Technology BIS Space Flight 1406MT_Contents.pdf, Cover.jpg 1407SF_Contents.pdf, Cover.jpg [What’s New in Real Library?] [謝辞] - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 2014.7.10 12:30 http://sankei.jp.msn.com/wired/ スマートフォンが国際宇宙ステーション・ロボットの頭脳に 7 月 11 日に ISS に向け打上げる宇宙船には、グーグル 3D ヴィジョン Satellites」(姿勢保持、連動、方向修正同期型実験衛星)の略で、 搭載スマホ「Tango」が積込まれる。ISS 船内で浮遊しながら飛行士た 将来的には、ISS 船外での危険作業を含め、宇宙飛行士の代わりに ちを支援するロボットに利用される。 日常雑務をこなせるようになることが期待されていた。ただし、2006 年に 初めて ISS に送込まれたときには、正確な浮遊動作をする以外に大し たことはできなかった。カリフォルニア州マウンテンヴューにある NASA のエ イムズ研究センタの研究者たちは、2010 年から、SPHERES を改良す る最も優れた方法を探すべく取組んできた。 悩んだ結果、スマホにた どり着いた。 「SPHERES 高度化プロジェクト・マネージャー」のクリス・プ ロヴェンチャーは、Reuters に次のように話している。「われわれは、通信 やカメラ、処理能力の向上、加速度計をはじめとする各種センサなどを NASA は 7 月 11 日(米時間)、ISS に向けて、グーグル新型スマートフ 追加したかった。どうすればよいか頭を悩ませていたときに、その答えは ォンを乗せた宇宙船を打上げ予定。3D ヴィジョン技術「Tango」(日本 自分たちの手の中にあったことに気づいた。つまり、スマートフォンを使お 語版記事) うということになったのだ」 グーグルの「Tango」技術を搭載したスマートフ http://wired.jp/2014/05/26/google-creating-project-tango-tablets-with ォンには、SPHERES が利用するための 3D マップの作成に使用できる -3d-computer-vision/ 赤外線深度センサなど、魅力的な多数の技術が搭載されている。もち -
ESD.00 Introduction to Systems Engineering, Lecture 3 Notes
Introduction to Engineering Systems, ESD.00 System Dynamics Lecture 3 Dr. Afreen Siddiqi From Last Time: Systems Thinking • “we can’t do just one thing” – things are interconnected and our actions have Decisions numerous effects that we often do not anticipate or realize. Goals • Many times our policies and efforts aimed towards some objective fail to produce the desired outcomes, rather we often make Environment matters worse Image by MIT OpenCourseWare. Ref: Figure 1-4, J. Sterman, Business Dynamics: Systems • Systems Thinking involves holistic Thinking and Modeling for a complex world, McGraw Hill, 2000 consideration of our actions Dynamic Complexity • Dynamic (changing over time) • Governed by feedback (actions feedback on themselves) • Nonlinear (effect is rarely proportional to cause, and what happens locally often doesn’t apply in distant regions) • History‐dependent (taking one road often precludes taking others and determines your destination, you can’t unscramble an egg) • Adaptive (the capabilities and decision rules of agents in complex systems change over time) • Counterintuitive (cause and effect are distant in time and space) • Policy resistant (many seemingly obvious solutions to problems fail or actually worsen the situation) • Char acterized by trade‐offs (h(the l ong run is often differ ent f rom the short‐run response, due to time delays. High leverage policies often cause worse‐before‐better behavior while low leverage policies often generate transitory improvement before the problem grows worse. Modes of Behavior Exponential Growth Goal Seeking S-shaped Growth Time Time Time Oscillation Growth with Overshoot Overshoot and Collapse Time Time Time Image by MIT OpenCourseWare. Ref: Figure 4-1, J. -
Lecture 9 – Modeling, Simulation, and Systems Engineering
Lecture 9 – Modeling, Simulation, and Systems Engineering • Development steps • Model-based control engineering • Modeling and simulation • Systems platform: hardware, systems software. EE392m - Spring 2005 Control Engineering 9-1 Gorinevsky Control Engineering Technology • Science – abstraction – concepts – simplified models • Engineering – building new things – constrained resources: time, money, • Technology – repeatable processes • Control platform technology • Control engineering technology EE392m - Spring 2005 Control Engineering 9-2 Gorinevsky Controls development cycle • Analysis and modeling – Control algorithm design using a simplified model – System trade study - defines overall system design • Simulation – Detailed model: physics, or empirical, or data driven – Design validation using detailed performance model • System development – Control application software – Real-time software platform – Hardware platform • Validation and verification – Performance against initial specs – Software verification – Certification/commissioning EE392m - Spring 2005 Control Engineering 9-3 Gorinevsky Algorithms/Analysis Much more than real-time control feedback computations • modeling • identification • tuning • optimization • feedforward • feedback • estimation and navigation • user interface • diagnostics and system self-test • system level logic, mode change EE392m - Spring 2005 Control Engineering 9-4 Gorinevsky Model-based Control Development Conceptual Control design model: Conceptual control sis algorithm: y Analysis x(t+1) = x(t) + -
Paper Session I-A - Liquid Rocket Boosters for Shuttle
The Space Congress® Proceedings 1989 (26th) Space - The New Generation Apr 25th, 2:00 PM Paper Session I-A - Liquid Rocket Boosters for Shuttle James E. Hughes Manager, LRB Studies, Marshall Space Flight Center, NASA Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Hughes, James E., "Paper Session I-A - Liquid Rocket Boosters for Shuttle" (1989). The Space Congress® Proceedings. 8. https://commons.erau.edu/space-congress-proceedings/proceedings-1989-26th/april-25-1989/8 This Event is brought to you for free and open access by the Conferences at Scholarly Commons. It has been accepted for inclusion in The Space Congress® Proceedings by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. LIQUID ROCKET BOOSTERS FOR SHUTTLE James E. Hughes, Manager LRB Studies Marshall Space Flight Center, NASA ABSTRACT The Liquid Rocket Booster study was initiated vehicles, and a pressure fed system, once by NASA to define an alternative to the Solid referred to as the "Big Dumb Booster". The Rocket Boosters used on the STS. These prime study contractors, Martin Marietta Cor studies have involved MSFC, JSC and KSC poration and General Dynamics Space Sys and their contractors. The prime study con tems, were assisted considerably by the ef tractors, Martin Marietta Corporation and forts of Lockheed Space Operations Co. General Dynamics Space Systems, have (LSOC) at the Kennedy Space Center and identified Liquid Booster configurations which Lockheed Engineering and Sciences Co. would replace the SRB's in the Shuttle stack. (LESC) at Johnson Space Center, as well as wind tunnel testing at MSFC, and other sup The Liquid Rocket Booster increases Shuttle port. -
+ Part 17: Acronyms and Abbreviations (265 Kb PDF)
17. Acronyms and Abbreviations °C . Degrees.Celsius °F. Degrees.Fahrenheit °R . Degrees.Rankine 24/7. 24.Hours/day,.7.days/week 2–D. Two-Dimensional 3C. Command,.Control,.and.Checkout 3–D. Three-Dimensional 3–DOF . Three-Degrees.of.Freedom 6-DOF. Six-Degrees.of.Freedom A&E. Architectural.and.Engineering ACEIT. Automated.Cost-Estimating.Integrated.Tools ACES . Acceptance.and.Checkout.Evaluation.System ACP. Analytical.Consistency.Plan ACRN. Assured.Crew.Return.Vehicle ACRV. Assured.Crew.Return.Vehicle AD. Analog.to.Digital ADBS. Advanced.Docking.Berthing.System ADRA. Atlantic.Downrange.Recovery.Area AEDC. Arnold.Engineering.Development.Center AEG . Apollo.Entry.Guidance AETB. Alumina.Enhanced.Thermal.Barrier AFB .. .. .. .. .. .. .. Air.Force.Base AFE. Aero-assist.Flight.Experiment AFPG. Apollo.Final.Phase.Guidance AFRSI. Advanced.Flexible.Reusable.Surface.Insulation AFV . Anti-Flood.Valve AIAA . American.Institute.of.Aeronautics.and.Astronautics AL. Aluminum ALARA . As.Low.As.Reasonably.Achievable 17. Acronyms and Abbreviations 731 AL-Li . Aluminum-Lithium ALS. Advanced.Launch.System ALTV. Approach.and.Landing.Test.Vehicle AMS. Alpha.Magnetic.Spectrometer AMSAA. Army.Material.System.Analysis.Activity AOA . Analysis.of.Alternatives AOD. Aircraft.Operations.Division APAS . Androgynous.Peripheral.Attachment.System APS. Auxiliary.Propulsion.System APU . Auxiliary.Power.Unit APU . Auxiliary.Propulsion.Unit AR&D. Automated.Rendezvous.and.Docking. ARC . Ames.Research.Center ARF . Assembly/Remanufacturing.Facility ASE. Airborne.Support.Equipment ASI . Augmented.Space.Igniter ASTWG . Advanced.Spaceport.Technology.Working.Group ASTP. Advanced.Space.Transportation.Program AT. Alternate.Turbopump ATCO. Ambient.Temperature.Catalytic.Oxidation ATCS . Active.Thermal.Control.System ATO . Abort-To-Orbit ATP. Authority.to.Proceed ATS. Access.to.Space ATV . Automated.Transfer.Vehicles ATV . -
Round Trip to Orbit: Human Spaceflight Alternatives
Round Trip to Orbit: Human Spaceflight Alternatives August 1989 NTIS order #PB89-224661 Recommended Citation: U.S. Congress, Office of Technology Assessment, Round Trip to Orbit: Human Spaceflight Alternatives Special Report, OTA-ISC-419 (Washington, DC: U.S. Government Printing Office, August 1989). Library of Congress Catalog Card Number 89-600744 For sale by the Superintendent of Documents U.S. Government Printing Office, Washington, DC 20402-9325 (order form can be found in the back of this special report) Foreword In the 20 years since the first Apollo moon landing, the Nation has moved well beyond the Saturn 5 expendable launch vehicle that put men on the moon. First launched in 1981, the Space Shuttle, the world’s first partially reusable launch system, has made possible an array of space achievements, including the recovery and repair of ailing satellites, and shirtsleeve research in Spacelab. However, the tragic loss of the orbiter Challenger and its crew three and a half years ago reminded us that space travel also carries with it a high element of risk-both to spacecraft and to people. Continued human exploration and exploitation of space will depend on a fleet of versatile and reliable launch vehicles. As this special report points out, the United States can look forward to continued improvements in safety, reliability, and performance of the Shuttle system. Yet, early in the next century, the Nation will need a replacement for the Shuttle. To prepare for that eventuality, NASA and the Air Force have begun to explore the potential for advanced launch systems, such as the Advanced Manned Launch System and the National Aerospace Plane, which could revolutionize human access to space. -
Large Reusable Liquid Rocket Booster
Determination of the Nose Cone Shape for a Large Reusable Liquid Rocket Booster by ROBERT LAUREN ACKER B.S., Massachusetts Institute of Technology 1987 SUBMITTED IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE DEGREE OF MASTER OF SCIENCE IN AERONAUTICS AND ASTRONAUTICS at the MASSACHUSETTS INSTITUTE OF TECHNOLOGY February 1988 ©Robert L. Acker 1988 The author hereby grants M.I.T. and Hughes Aircraft Company permission to reproduce and to distribute copies of this thesis document in whole or in part. Signature of Author Department of Aeronautics and Astronautics January 12, 1988 Reviewed by C. P. Rubin Hughes Aircraft Company Certified by - rv -- - Prof. Walter M. Hollister Thesis Supervisor, Deprtment of Aeronautics and Astronautics Accepted by , {"' Prof. Harold Y. Wachman Chairman, Department Graduate Committee Department of Aeronautics and Astronautics MASSACHUSETTSINST:7, a OF TECHNOLOGY WHDAWN I FEB 0 4198 M.LT.W LIB-RAiES , J Determination of the Nose Cone Shape for a Large Reusable Liquid Rocket Booster by Robert L. Acker Submitted to the Department of Aeronautics and Astronautics in partial fulfillment of the requirements for the degree of Master of Science in Aeronautics and Astronautics January 15, 1988 Abstract Recently there has been a lot of interest in making reusable space vehicles in an effort to lower launch costs. In addition, the use of liquid propellant in a multistage vehicle provides for the maximum performance. This study examines the forces on the nose cone of the first stage of such a rocket and uses them to determine the best shape for the nose cone. The specific stage looked at is a strap-on booster on a design proposed at Hughes Aircraft Company.