Human Rating Requirements for NASA’s Constellation Program Presented by Debbie Berdich Aerospace Medical Association (AsMA) 80 th Annual Scientific Meeting.

Slides:



Advertisements
Similar presentations
Museum Presentation Intermuseum Conservation Association.
Advertisements

Technology Module: Technology Readiness Levels (TRLs) Space Systems Engineering, version 1.0 SOURCE INFORMATION: The material contained in this lecture.
Business Continuity Training & Awareness by Sulia Toutai (ANZ)
System Integration Verification and Validation
More CMM Part Two : Details.
Software Modeling SWE5441 Lecture 3 Eng. Mohammed Timraz
USING NASA QUALITY STANDARDS NASA Academy of Aerospace (AAQ) Quality Mini-Workshop Ken Crane Quality Engineering Technical Discipline Team Lead NASA SAFETY.
Lunar Advanced Science and Exploration Research: Partnership in Science and Exploration Michael J. Wargo, Sc.D. Chief Lunar Scientist for Exploration Systems.
National Aeronautics and Space Administration Commercial Crew Program (CCP) Key Paradigm Changes Presenter Title Date of Presentation Philip McAlister.
National Aeronautics and Space Administration Commercial Crew Initiative Overview and Status to the COMSTAC Philip McAlister NASA Exploration Systems Mission.
TRAINING AND DRILLS. Training and Drills Ensure A comprehensive, coordinated, and documented program as an integral part of the emergency management program.
Human Systems Engineering Concentration Amy Bayes 15 October 2014.
1 Human / Systems Integration (HSI) Tools for NASA Systems Engineering David J. Fitts Chief, Habitability & Human Factors Branch, NASA/JSC HSIS 2009 March.
Development plan and quality plan for your Project
Software Verification and Validation (V&V) By Roger U. Fujii Presented by Donovan Faustino.
PART IX: EMERGENCY EXPOSURE SITUATIONS Module IX.1: Generic requirements for emergency exposure situations Lesson IX.1-2: General Requirements Lecture.
Introduction to Human Factors and the Human Centered Design Process
Codex Guidelines for the Application of HACCP
PMSS Final SOW May 22 nd, Statement of Work 2 GLENN RESEARCH CENTER PROJECT MANAGEMENT SUPPORT SERVICES (PMSS) The Contractor shall provide expert.
Effective Methods for Software and Systems Integration
EHS Management System Elements
The Pursuit for Efficient S/C Design The Stanford Small Sat Challenge: –Learn system engineering processes –Design, build, test, and fly a CubeSat project.
1 Addressing Common EHR Implementation Problems June 18, 2010 Tammy Geltmaker, RN, BSN, MHA EHR Consulting Manager, Health Care Excel Bonnie Hollopeter,
S/W Project Management Software Process Models. Objectives To understand  Software process and process models, including the main characteristics of.
Introduction to RUP Spring Sharif Univ. of Tech.2 Outlines What is RUP? RUP Phases –Inception –Elaboration –Construction –Transition.
Chapter 2 The process Process, Methods, and Tools
1 PANEL: NASA Human/Systems Integration (HSI) Presentation: Human-Centered Design Capability David J. Fitts Chief, Habitability & Human Factors Branch,
Unit 8:COOP Plan and Procedures  Explain purpose of a COOP plan  Propose an outline for a COOP plan  Identify procedures that can effectively support.
Introduction to ISO 9001:2000.
IAEA International Atomic Energy Agency Reviewing Management System and the Interface with Nuclear Security (IRRS Modules 4 and 12) BASIC IRRS TRAINING.
Slide 1Lesson 14: Fundamentals of the CAP Flying Safety Program Fundamentals of the CAP Flying Safety Program.
DESIGNING FOR SAFETY CHAPTER 9. IMPORTANCE OF DESIGNING FOR SAFETY  In the near future, the level of safety that companies and industries achieve will.
Certification and Accreditation CS Phase-1: Definition Atif Sultanuddin Raja Chawat Raja Chawat.
Human Factors (HF) - Assessment Method Agenda What is Human Factors? Why do we need HF-Assessment Method ? What is the HF-Assessment Method ? Why.
The ISECG Global Exploration Roadmap Status update at Target NEO2 Workshop July 9, 2013 NASA/Kathy Laurini Human Exploration & Ops Mission Directorate.
Slide 1V&V 10/2002 Software Quality Assurance Dr. Linda H. Rosenberg Assistant Director For Information Sciences Goddard Space Flight Center, NASA
CHECKPOINTS OF THE PROCESS Three sequences of project checkpoints are used to synchronize stakeholder expectations throughout the lifecycle: 1)Major milestones,
LSST Camera CD-3 Review Brookhaven National Laboratory, Brookhaven, NY LSST Safety Council Camera Review Bremerton, WA 2015 LSST Camera Environment,
Notes of Rational Related cyt. 2 Outline 3 Capturing business requirements using use cases Practical principles  Find the right boundaries for your.
1 PANEL: NASA Human / Systems Integration (HSI) Presentation: HSI in the Program Life Cycle David J. Fitts Chief, Habitability & Human Factors Branch,
RASC-AL 2010 Topics. TECHNOLOGY-ENABLED HUMAN MARS MISSION NASA is interested in eventual human mission to the Martian surface. Current Mars design reference.
Unit 6 Lesson 1 Explanation. In 2004, President Bush set the following goal for the NASA constellation program, “this vision… is a sustainable and affordable.
SE&I Pre-Proposal Meeting GSFC - JPL Systems Engineering Management Colleen McGraw.
Constellation Space Transportation Planning Office July 30, 2009.
Intelligent Systems Software Assurance Symposium 2004 Bojan Cukic & Yan Liu, Robyn Lutz & Stacy Nelson, Chris Rouff, Johann Schumann, Margaret Smith July.
Environment and Disaster Planning Hari Srinivas, GDRC Rajib Shaw, Kyoto University Contents of the presentation: -What is the problem? -Precautionary Principles.
Decision Making Process Program Planning and Control Deana Hackfeld Management Systems Office November 17, 2006.
Solar Probe Plus A NASA Mission to Touch the Sun March 2015 Instrument Suite Name Presenter's Name.
The Second Annual Medical Device Regulatory, Reimbursement and Compliance Congress Presented by J. Glenn George Thursday, March 29, 2007 Day II – Track.
Process Asad Ur Rehman Chief Technology Officer Feditec Enterprise.
 CMMI  REQUIREMENT DEVELOPMENT  SPECIFIC AND GENERIC GOALS  SG1: Develop CUSTOMER Requirement  SG2: Develop Product Requirement  SG3: Analyze.
SRR and PDR Charter & Review Team Linda Pacini (GSFC) Review Chair.
Approved For Public Release © The Aerospace Corporation 2009 June 17, 2009 Initial Summary of Human Rated Delta IV Heavy Study Briefing to the Review of.
Safety & Health Considerations in Accommodating Commercial Activties David Loyd, JSC Safety & Test Operations 2013 NASA Safety Directors & Occupational.
Probabilistic Risk Assessment and Conceptual Design Bryan C Fuqua – SAIC Diana DeMott – SAIC
SwCDR (Peer) Review 1 UCB MAVEN Particles and Fields Flight Software Critical Design Review Peter R. Harvey.
Information Technology Project Management, Seventh Edition.
Info-Tech Research Group1 Info-Tech Research Group, Inc. Is a global leader in providing IT research and advice. Info-Tech’s products and services combine.
1 Design and evaluation methods: Objectives n Design life cycle: HF input and neglect n Levels of system design: Going beyond the interface n Sources of.
DoD Template for Application of TLCSM and PBL
Product Validation Adapted from the NASA Systems Engineering Handbook for CSULB EE 400D by Alia Bonetti.
Identify the Risk of Not Doing BA
Software Independent Verification and Validation (IV&V)
Air Carrier Continuing Analysis and Surveillance System (CASS)
How S-18 processes help make systems trustworthy
Instrument PDR Summary of Objectives
PSS verification and validation
Jeff Dutton/NASA COR August 26, 2019
Presentation transcript:

Human Rating Requirements for NASA’s Constellation Program Presented by Debbie Berdich Aerospace Medical Association (AsMA) 80 th Annual Scientific Meeting 05 May2009 Los Angeles, California Panel : The Process to Keep the Human in Human Space Flight

Requirements Development Research How can we do better? Operations Lessons learned! Design Hands-on architectural involvement Human System Integration Process Requirements Integration Negotiating project buy-in Verification Were requirements met?

3 NASA Constellation Program (CxP) - Projects CxP ProjectLead NASA Center Developmental PhaseOperational Phase Crew Exploration Vehicle – CEV (Orion) JSCDevelop and test Orion spacecraft to transport crew to and from space Provide Orion spacecraft AresMSFCDevelop and test Ares I and Ares V launch vehicles Provide Ares launch vehicles Ground OperationsKSCPerform ground processing and integrated testing of launch vehicles. Plan, construct and/or reconfigure integration, launch, and recovery services for Orion Crew Module, Ares I, and Ares V Provide logistics and launch services. Provide post-landing and recovery services for the crew, Orion Crew Module, and spent Ares Solid Rocket Boosters. Mission OperationsJSCConfigure, test, plan, and operate facilities, systems, and procedures. Plan missions and flight operations Train crew, flight controllers, and support staff. Coordinate crew operations during missions. Lunar Lander (Altair)JSCDevelop and test the Lunar Lander to transport crew to and from the lunar surface and to provide a habitable volume for initial lunar missions Provide Lunar Lander Extravehicular Activities (EVA) Systems JSCDevelop EVA systems (spacesuits, tools, and servicing and support equipment) to support crew survival during launch, atmosphere entries, landing, abort scenarios, and outside the space vehicle and on the lunar surface. Provide spacesuits and tools Lunar Surface SystemsJSCDevelop Lunar Surface Systems (equipment and systems for crew operation on the lunar surface) such as habitats, rovers, and construction systems Provide Lunar Surface Systems Table adapted from FORMULATION OF NASA’s CONSTELLATION PROGRAM, Oct 2007

HSI in NASA’s Constellation Program (CxP) via Human Rating Requirements - NPR B The purpose of NASA Procedural Requirements (NPR) B, Human Rating Requirements (HRR) document, is to define and implement the additional processes, procedures, and requirements necessary to produce human-rated space systems that protect the safety of crew members and passengers on NASA space missions. A human-rated system accommodates human needs, effectively utilizes human capabilities, controls hazards and manages safety risk associated with human spaceflight, and provides, to the maximum extent practical, the capability to safely recover the crew from hazardous situations. Human-rating is an integral part of all program activities throughout the life cycle of the system, including design and development; test and verification; program management and control; flight readiness certification; mission operations; sustaining engineering; maintenance/upgrades; and disposal. The NPR is not levied directly on any of the Projects. Instead, CxP generates requirements which will meet the intent of the NPR and then flows those down to the Projects via allocation matrices.

5 Relationship of NASA Standards to HSIR Human-Systems Integration Requirements – HSIR (CxP Rev C) – Defines parameters of a habitable environment, capabilities and limitations of the flight and ground crew that drive the design of the CxP Architecture systems to achieve mission objectives, and provides the parameters that protect the health and safety of the crew and allows them to perform their functions in an efficient and effective manner Key mechanism to achieve human rating Enables proper integration of human-to-system interfaces for all mission phases Applicability matrix allows allocation down to each project as appropriate – Focuses on proper integration of human-to-system interfaces for all mission phases through applicable requirements. Human Rating (NPR B) Authority NASA Std 3001 Vol 1, 2 Knowledge HSIR (CxP 70024) Constellation Requirements Benchmark of capabilities for human-rated space systems Directs CxP to evaluate crew workload, conduct human-in-the-loop usability evaluations, perform human error analysis, prove that integrated human-system performance test results were used to validate the system design Focuses primarily on the integration of the human into the system to prevent catastrophic events during the mission Defines levels of acceptable crew health and performance risks resulting from spaceflight. Volume 1 sets standards related to crew health. Volume 2 defines the environmental, habitability, and human factors standards related to environmental health and human-system interfaces

Human Rating Requirements Flow Down Example - Handling Qualities Human-Rating Requirements for Space Systems (NPR B) -HRR – HRR mandates the crew’s ability to effectively control the spacecraft when necessary for mission completion or to prevent a catastrophic event. It calls out an “accepted standard”, Handling Qualities (HQ) for manual control of flight path and attitude Names Cooper Harper Rating Scale as the means to measure handling quality – NPR requires that the Project determine and present proof of how the HQ requirements are integrated into system design, how to evaluate the design, leading to eventual verification and validation. (1) Human-rating is the process of designing, evaluating, and assuring that the total system can safely conduct the required human missions. (2) Human-rating includes the incorporation of design features and capabilities that accommodate human interaction with the system to enhance overall safety and mission success. (3) Human-rating includes the incorporation of design features and capabilities to enable safe recovery of the crew from hazardous situations [3.4.2] The crewed spacecraft shall exhibit Level 1 handling qualities (Handling Qualities Rating (HQR) 1, 2 and 3), as defined by the Cooper-Harper Rating Scale, during manual control of the spacecraft’s flight path and attitude

Tracing Requirements - Human Rating to HSIR In the Example of Handling Qualities Human Systems Integration Requirements (HSIR) CxP Rev C – HSIR has two requirements for Handling Qualities – allocated to Orion (CEV) and Altair (Lunar Lander) One requirement for Loss of crew or vehicle; One for Loss of mission Verification specified as analysis and test – Task based and via Cooper Harper Rating Scale [HS7003] The system shall have handling quality ratings of 1 or 2 on the Cooper-Harper Scale for tasks that can result in loss of crew or loss of vehicle. [HS7003V] The crew-safety handling quality rating shall be verified by analysis and test. The analysis (task analysis) shall identify the list of tasks in which errors can result in loss of crew or loss of vehicle. The test shall consist of at least 5 crew trained as operators performing the listed control tasks in a flight-like simulator or mockup and providing handling-quality ratings on the Cooper-Harper scale. The verification shall be considered successful when the analysis with test shows that, for all tasks that could result in crew or vehicle loss, no individual Cooper-Harper rating exceeds 2. [HS7004] The system shall have handling quality ratings of 1, 2 or 3 on the Cooper Harper Scale for tasks that can result in loss of mission. [HS7004V] The mission-safety handling quality rating shall be verified by analysis and test. The analysis (task analysis) shall identify the list of tasks in which errors can result in loss of mission. The test shall consist of at least 5 crew trained as operators performing the listed control tasks in a flight-like simulator or mockup and providing handling-quality ratings on the Cooper-Harper scale. The verification shall be considered successful when the analysis with test shows that, for all tasks that could result in mission loss, no individual Cooper-Harper rating exceeds 3.

8 Integration of Handling Qualities Requirements Orion (CEV)Project established a Handling Qualities Working Group (WG) to determine how the handling qualities requirements could be addressed early in the design and throughout the life cycle as the design matures. WG is an integrated team with participation by key stakeholders including vehicle designers, mission operations, crew office, human engineering, mockup developers, etc – Credible scenarios are generated to scope limits on when the handling qualities requirements apply – Decisions are made on when and how human in the loop tests will be conducted – Hardware and software availability and fidelity is determined – Simulation software fidelity for flight vehicle dynamics including Guidance, Navigation, and Control (GN&C) algorithms is established – Mockup state of readiness and availability is assessed Figure courtesy G. Vos Orion Spacecraft Handling Qualities System Baseline Review 12/11/08 Prototype Input Device Hardware

9 Integration of Handling Qualities Requirements The Orion Project’s iterative design approach allows the stakeholders to be engaged in the integration of the HQ requirements into vehicle and mission design. Such an approach also buys down risk of loss of crew or loss of mission due to inadequate handling qualities – The risk management is part of the design process and the steps to mitigate identified risks are focused on reducing either likelihood that the event will occur or the consequences if it does occur From NPR B Human Rating Requirements (HRR) document …. Above all, human-rating is more than a set of requirements, a process, or a certification – it involves a mindset, instilled by leadership, where each person feels personally responsible for their piece of the design and for the safety of the crew.