Repository logo
Log in(current)
Repository logoMIT Open ScholarshipDSpace@MIT
  1. Home
  2. MIT Open Access Articles
  3. MIT Open Access Articles
  4. A New Approach to Hazard Analysis for Rotorcraft

A New Approach to Hazard Analysis for Rotorcraft

Thumbnail Image
Download
Name

AHS-final.pdf

Size

1.24 MB

Format

Adobe PDF

Checksum (MD5)

7d0b39b44eda6e12e14d297ba6b31283

Download all files submitted through automated deposit
sword-2018-04-02.original.zip (1.15 MB)
Author(s)
Arterburn, Dave
•
Abrecht, Blake Ryan
•
Horney, David Craig
•
Schneider, Jonathan James
•
Abel, Brandon Ross
•
Leveson, Nancy G
Date Issued
February 2016
Journal
Specialists' Meeting on Development, Affordability and Qualification of Complex Systems 2016
Publisher
American Helicopter Society International
Citation
Abrecht, Blake et al. "A New Approach to Hazard Analysis for Rotorcraft." Specialists' Meeting on Development, Affordability and Qualification of Complex Systems 2016, 9-10 February, 2016, Huntsville, Alabama, American Helicopter Society International, 2016.
Version
Author's final manuscript
Abstract
STPA is a new hazard analysis technique that can identify more hazard causes than traditional techniques. It is based on the assumption that accidents result from unsafe control rather than component failures. To demonstrate and evaluate STPA for its application to rotorcraft, it was used to analyze the UH-60MU Warning, Caution, and Advisory (WCA) system associated with the electrical and fly-by-wire flight control system (FCS). STPA results were compared with an independently conducted hazard analysis of the UH-60MU using traditional safety processes described in SAE ARP 4761 and MIL-STD-882E. STPA found the same hazard causes as the traditional techniques and also identified things not found using traditional methods, including design flaws, human behavior, and component integration and interactions. The analysis includes organizational and physical components of systems and can be used to design safety into the system from the beginning of development while being compliant with MIL-STD-882. Copyright 2016 by American Helicopter Society International All right reserved.
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Massachusetts Institute of Technology. Institute for Data, Systems, and Society
Terms of Use
Creative Commons Attribution-Noncommercial-Share Alike
http://creativecommons.org/licenses/by-nc-sa/4.0/
Persistent DSpace Link
http://hdl.handle.net/1721.1/114753
DOI of Published Version
http://toc.proceedings.com/31579webtoc.pdf
Repository logo
PrivacyPermissionsAccessibilityContact us
Repository logo
Notify us about copyright concerns.