Small UAV SHM System Functional Hazard Analysis-Reference-Cited by-同舟云学术

Small UAV SHM System Functional Hazard Analysis

Published:2021-06-01 Issue:2 Volume:51 Page:33-41
ISSN:2083-4608
Container-title:Journal of KONBiN
language:en
Short-container-title:

Author:

Klimaszewski Sławomir¹,Sajda Krzysztof¹,Szawłowski Sergiusz¹

Affiliation:

1. Air Force Institute of Technology

Abstract

Abstract The safety assessment process tailored to Remotely Piloted Aircraft Systems (RPAS) applications has been discussed briefly. The modified Hazard Reference System for STANAG 4703 Category UAV including Non Safety Effect (NSE) severity category has been proposed. The Functional Hazard Analysis (FHA) for small Unmanned Aerial Vehicle (UAV) Structural Health Monitoring (SHM) system has been conducted.

Publisher

Walter de Gruyter GmbH

Subject

Safety, Risk, Reliability and Quality

Link

https://www.sciendo.com/pdf/10.2478/jok-2021-0020

Reference10 articles.

1. 1. ATA MSG-3. Operator/Manufacturer Scheduled Maintenance Development”, Volume 1 - Fixed Wing Aircraft. ATA. Revision 2018.1.

2. 2. AC 23.1309-1E - System Safety Analysis and Assessment for Part 23 Airplanes, Federal Aviation Administration. November 2011.

3. 3. MIL-STD-882E. Department of Defense Standard Practice. System Safety. US Department of Defense. May 2012.

4. 4. MIL-STD-1530D (w/CHANGE-1), Department of Defense Standard Practice: Aircraft Structural Integrity Program (ASIP). Department of Defense. October 2016.

5. 5. NATO STANDARD AEP-83. Light Unmanned Aircraft Systems Airworthiness Requirements, Edition B Version 1. NATO. November 2016.

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