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IV&V Assurance Case Design for Artemis IIAs human-rated missions like those in NASA’s Artemis program continue to grow in both size and complexity, and the role of software in achieving mission objectives expands dramatically, NASA’s Independent Verification and Validation (IV&V) Teams face evolving challenges in assuring the safety and performance of the safety- and mission-critical embedded software that is essential to landing astronauts on the surface of the Moon by 2024. Key among these challenges is IV&V’s desire to present a cohesive, integrated assurance statement to its stakeholders that encapsulates and summarizes our assurance positions across the integrated Artemis systems and their combined role in support of a safe and successful flight. In order to meet this challenge, the IV&V Teams have begun a transition to using formal assurance case concepts and documentation in the Goal Structuring Notation (GSN) to build an argument in support of software assurance. IV&V recognizes significant benefits to the logical argumentation structure provided by assurance cases and GSN over our current practices for documenting and managing assurance claims. In order to reap these benefits, IV&V is integrating the use of assurance case concepts with our paradigm of follow-the-risk capability based assurance. Because of this, assurance cases created and used by IV&V are distinct from the sort of assurance case created by a development project or embedded software assurance organization. IV&V’s assurance cases depend much less upon standards and regulations, and more on evidence captured by IV&V regarding the environment, requirements, design, and implementation. IV&V constructs an independent network of claims based on an independent decomposition of arguments. Based upon the risk posture of these claims and their associated software and software artifacts, IV&V then develops and executes engineering analyses and testing, which provide evidence to either support or refute the claim. This emerging risk-informed assurance case methodology is being put into practice as IV&V plans for support of the Artemis II mission, the first flight of the Orion capsule and Space Launch System with astronauts on board.
Document ID
20200001646
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Gerek Whitman
(TASC (United States) Chantilly, Virginia, United States)
Paul Amoroso
(Technology Management Company (United States) Albuquerque, New Mexico, United States)
Gregory Black
(TASC (United States) Chantilly, Virginia, United States)
Deneen Marculaitis-Granger
(Engility (United States) Chantilly, Virginia, United States)
Justin Smith
(Katherine Johnson Independent Verification and Validation Facility Fairmont, West Virginia, United States)
John Bradbury
(Engility (United States) Chantilly, Virginia, United States)
Wes Deadrick
(Katherine Johnson Independent Verification and Validation Facility Fairmont, West Virginia, United States)
Date Acquired
March 16, 2020
Publication Date
August 21, 2020
Publication Information
Publication: 2020 IEEE Aerospace Conference
Publisher: Institute of Electrical and Electronics Engineers
ISSN: 1095-323X
ISBN: 9781728127354
e-ISBN: 9781728127347
Subject Category
Quality Assurance And Reliability
Report/Patent Number
GSFC-E-DAA-TN76738
Meeting Information
Meeting: 41st International IEEE Aerospace Conference
Location: Big Sky, MT
Country: US
Start Date: March 7, 2020
End Date: March 14, 2020
Sponsors: American Institute of Aeronautics and Astronautics, Prognostics and Health Management Society, Institute of Electrical and Electronics Engineers
Funding Number(s)
CONTRACT_GRANT: NNG17SA26C
Distribution Limits
Public
Copyright
Public Use Permitted.
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