2020 IEEE Systems Security Symposium (SSS) 2020
DOI: 10.1109/sss47320.2020.9197728
|View full text |Cite
|
Sign up to set email alerts
|

A STPA-Sec Case Study: Eliciting Early Security Requirements for a Small Unmanned Aerial System

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1

Citation Types

0
3
0

Year Published

2021
2021
2025
2025

Publication Types

Select...
3
2

Relationship

0
5

Authors

Journals

citations
Cited by 5 publications
(3 citation statements)
references
References 4 publications
0
3
0
Order By: Relevance
“…STPA-Sec has been successively applied in a variety of sectors. In [31] STPA-Sec is used to guide the choice of security requirements for the design of a drone. The analysis is made upon three different levels of detail to provide traceability to the system owner's mission, to make systems security easily understandable.…”
Section: Literature Reviewmentioning
confidence: 99%
“…STPA-Sec has been successively applied in a variety of sectors. In [31] STPA-Sec is used to guide the choice of security requirements for the design of a drone. The analysis is made upon three different levels of detail to provide traceability to the system owner's mission, to make systems security easily understandable.…”
Section: Literature Reviewmentioning
confidence: 99%
“…Thus, a platform-centric SA is proposed, instead of relying on human pilots' perceptions as in [10]. The paper also innovates since IFA 2 S design is completely based on Systems-Theoretic Process Analysis (STPA) method [11] [12], aiming to allow the system to act as soon as it identifies a situation that potentially leads to an accident. This paper describes a process similar to that found in articles [13] and [14] to achieve SA in dynamic systems.…”
Section: Related Workmentioning
confidence: 99%
“…Measurements were performed on the variable ξ (either vertical speed, h  , or roll angle, φ ) and verified if 20 consecutive standard deviation measurements, T N , are above a certain level, Lim T N . Number of samples was determined empirically during simulations, taking into account the capability of the system for identifying turbulences efficiently, avoiding both false alarmsand aircraft dangerous attitudes as defined in(11) and(12).…”
mentioning
confidence: 99%