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BSI 23/30479099 DC 2023

BSI 23/30479099 DC 2023

$13.70

BS EN 4709-006. Aerospace series. Unmanned Aircraft Systems – Part 006. Means to terminate flight, requirements, and verification

Published By Publication Date Number of Pages
BSI 2023 43
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PDF Catalog

PDF Pages PDF Title
7 1 Scope
2 Normative references
8 3 Terms and definitions
11 4 Product requirements and compliance of means to terminate the flight for Class 5 UAS
4.1 Reliability, predictability, and independence
4.1.1 Performance requirements
4.1.2 Verification method
4.1.2.1 Requirement (1) – Reliability
15 4.1.2.2 Requirement (2) – Predictability
4.1.2.3 Requirement (3) – Independence
17 4.1.3 Pass criteria
18 4.2 Descent performance
4.2.1 Performance requirements
4.2.2 Verification methods
4.2.2.1 Requirement (1) – Means
23 4.2.2.2 Requirement (2) – Sequence is automated
24 4.2.2.3 Requirement (3) – Prevention of powered horizontal displacement
4.2.2.4 Requirement (4) – Speed of descent and distance travelled
25 4.2.3 Pass criteria
4.3 Means to reduce the effect of UA impact dynamics
4.3.1 Performance requirements
26 4.3.2 Verification method
4.3.2.1 Requirement (1) – Reduction of effects of impact dynamics
4.3.2.2 Requirement (2) – Sequence is automated
4.3.2.3 Requirement (3) – Instructions to maintain
4.3.3 Pass criteria
4.4 Manufacturer’s instructions
27 5 Product requirements and compliance of means to terminate the flight for class 6 UAS
5.1 Reliability, predictability, and independence
5.2 Descent performance
5.2.1 General
5.2.2 Performance requirements
5.2.3 Verification methods
5.2.3.1 Requirement (4) – Speed of descent and distance travelled
5.2.4 Pass criteria
5.3 Manufacturer’s instructions
5.3.1 Requirements
28 5.3.2 Verification method – Part H: flight termination
5.3.2.1 Requirement (1) – Flight termination description
29 5.3.2.2 Requirement (2) –Pre-flight test
5.3.2.3 Requirement (3) – Minimum ground risk buffer
5.3.3 Pass criteria
30 Annex A (informative)Example design patterns for the representation of independent means to terminate flight (flight termination system) implementation
A.1 Example design patterns
33 A.2 Recommendations for the presentation of the UAS architecture
A.3 Abbreviations
34 Annex B (informative)Generic safety assessment
B.1 General
B.2 Approach
B.3 Checklist
37 Annex C (informative)Automation
39 Annex D (informative)Methods to perform descent and limit the effects of impact dynamics (semantic model)
D.1 Overview of typical methods to bring the UA to ground
D.2 Initiation
40 D.3 Descent
D.3.1 Controlled descent, if possible
D.3.2 Uncontrolled descent
41 D.3.3 Descent by parachute
D.4 Alight
D.5 Post-landing/post-impact
42 Annex ZA (informative)Relationship between this document and the essential requirements of Delegated regulation (EU) 2019/945 of 12th March 2019 on unmanned aircraft systems and on third-country operators of unmanned aircraft systems aimed to be covered

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