ASTM F 3201 : 2016
Current
The latest, up-to-date edition.
Standard Practice for Ensuring Dependability of Software Used in Unmanned Aircraft Systems (UAS)
Hardcopy , PDF
English
09-01-2016
CONTAINED IN VOL. 15.11, 2016 Specifies the dependability of UAS software.
Committee |
F 38
|
DocumentType |
Standard Practice
|
Pages |
11
|
PublisherName |
American Society for Testing and Materials
|
Status |
Current
|
1.1This standard practice intends to ensure the dependability of UAS software. Dependability includes both the safety and security aspects of the software.
1.2This practice will focus on the following areas: (a) Organizational controls (for example, management, training) in place during software development. (b) Use of the software in the system, including its architecture and contribution to overall system safety and security. (c) Metrics and design analysis related to assessing the code. (d) Techniques and tools related to code review. (e) Quality assurance. (f) Testing of the software.
1.3There is interest from industry and some parts of the CAAs to pursue an alternate means of compliance for software assurance for small UAS (sUAS).
1.4This practice is intended to support sUAS operations. It is assumed that the risk of sUAS will vary based on concept of operations, environment, and other variables. The fact that there are no souls onboard the UAS may reduce or eliminate some hazards and risks. However, at the discretion of the CAA, this practice may be applied to other UAS operations.
1.5This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.
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ASTM F 3298 : 2018 | Standard Specification for Design, Construction, and Verification of Fixed-Wing Unmanned Aircraft Systems (UAS) |
ASTM F 3196 : 2018 | Standard Practice for Seeking Approval for Beyond Visual Line of Sight (BVLOS) Small Unmanned Aircraft System (sUAS) Operations |
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RTCA DO 278 : A2011 | SOFTWARE INTEGRITY ASSURANCE CONSIDERATIONS FOR COMMUNICATION, NAVIGATION, SURVEILLANCE AND AIR TRAFFIC MANAGEMENT (CNS/ATM) SYSTEMS |
RTCA DO 178 : C2011 | SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION |
ICAO 9859 : 2013 | SAFETY MANAGEMENT MANUAL (SMM) |
RTCA DO 326 : A2014 | AIRWORTHINESS SECURITY PROCESS SPECIFICATION |
IEC 62304:2006+AMD1:2015 CSV | Medical device software - Software life cycle processes |
MIL-STD-882 Revision E:2012 | System Safety |
FAA AC 23.1309-1 : 2011 | SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES |
ISO 9001:2015 | Quality management systems — Requirements |
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