| PDF Pages<\/th>\n | PDF Title<\/th>\n<\/tr>\n | ||||||
|---|---|---|---|---|---|---|---|
| 7<\/td>\n | 1 Scope 2 Normative references <\/td>\n<\/tr>\n | ||||||
| 8<\/td>\n | 3 Terms and definitions <\/td>\n<\/tr>\n | ||||||
| 11<\/td>\n | 4 Product requirements and compliance of means to terminate the flight for Class\u00a05 UAS 4.1 Reliability, predictability, and independence 4.1.1 Performance requirements 4.1.2 Verification method 4.1.2.1 Requirement (1) \u2013 Reliability <\/td>\n<\/tr>\n | ||||||
| 15<\/td>\n | 4.1.2.2 Requirement (2) \u2013 Predictability 4.1.2.3 Requirement (3) \u2013 Independence <\/td>\n<\/tr>\n | ||||||
| 17<\/td>\n | 4.1.3 Pass criteria <\/td>\n<\/tr>\n | ||||||
| 18<\/td>\n | 4.2 Descent performance 4.2.1 Performance requirements 4.2.2 Verification methods 4.2.2.1 Requirement (1) \u2013 Means <\/td>\n<\/tr>\n | ||||||
| 23<\/td>\n | 4.2.2.2 Requirement (2) \u2013 Sequence is automated <\/td>\n<\/tr>\n | ||||||
| 24<\/td>\n | 4.2.2.3 Requirement (3) \u2013 Prevention of powered horizontal displacement 4.2.2.4 Requirement (4) \u2013 Speed of descent and distance travelled <\/td>\n<\/tr>\n | ||||||
| 25<\/td>\n | 4.2.3 Pass criteria 4.3 Means to reduce the effect of UA impact dynamics 4.3.1 Performance requirements <\/td>\n<\/tr>\n | ||||||
| 26<\/td>\n | 4.3.2 Verification method 4.3.2.1 Requirement (1) \u2013 Reduction of effects of impact dynamics 4.3.2.2 Requirement (2) \u2013 Sequence is automated 4.3.2.3 Requirement (3) \u2013 Instructions to maintain 4.3.3 Pass criteria 4.4 Manufacturer\u2019s instructions <\/td>\n<\/tr>\n | ||||||
| 27<\/td>\n | 5 Product requirements and compliance of means to terminate the flight for class\u00a06 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) \u2013 Speed of descent and distance travelled 5.2.4 Pass criteria 5.3 Manufacturer\u2019s instructions 5.3.1 Requirements <\/td>\n<\/tr>\n | ||||||
| 28<\/td>\n | 5.3.2 Verification method \u2013 Part H: flight termination 5.3.2.1 Requirement (1) \u2013 Flight termination description <\/td>\n<\/tr>\n | ||||||
| 29<\/td>\n | 5.3.2.2 Requirement (2) \u2013Pre-flight test 5.3.2.3 Requirement (3) \u2013 Minimum ground risk buffer 5.3.3 Pass criteria <\/td>\n<\/tr>\n | ||||||
| 30<\/td>\n | Annex\u00a0A (informative)Example design patterns for the representation of independent means to terminate flight (flight termination system) implementation A.1 Example design patterns <\/td>\n<\/tr>\n | ||||||
| 33<\/td>\n | A.2 Recommendations for the presentation of the UAS architecture A.3 Abbreviations <\/td>\n<\/tr>\n | ||||||
| 34<\/td>\n | Annex\u00a0B (informative)Generic safety assessment B.1 General B.2 Approach B.3 Checklist <\/td>\n<\/tr>\n | ||||||
| 37<\/td>\n | Annex\u00a0C (informative)Automation <\/td>\n<\/tr>\n | ||||||
| 39<\/td>\n | Annex\u00a0D (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 <\/td>\n<\/tr>\n | ||||||
| 40<\/td>\n | D.3 Descent D.3.1 Controlled descent, if possible D.3.2 Uncontrolled descent <\/td>\n<\/tr>\n | ||||||
| 41<\/td>\n | D.3.3 Descent by parachute D.4 Alight D.5 Post-landing\/post-impact <\/td>\n<\/tr>\n | ||||||
| 42<\/td>\n | Annex\u00a0ZA (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 <\/td>\n<\/tr>\n<\/table>\n","protected":false},"excerpt":{"rendered":" BS EN 4709-006. Aerospace series. Unmanned Aircraft Systems – Part 006. Means to terminate flight, requirements, and verification<\/b><\/p>\n |