{"id":450690,"date":"2024-10-20T09:13:18","date_gmt":"2024-10-20T09:13:18","guid":{"rendered":"https:\/\/pdfstandards.shop\/product\/uncategorized\/bs-iso-53052024\/"},"modified":"2024-10-26T17:10:53","modified_gmt":"2024-10-26T17:10:53","slug":"bs-iso-53052024","status":"publish","type":"product","link":"https:\/\/pdfstandards.shop\/product\/publishers\/bsi\/bs-iso-53052024\/","title":{"rendered":"BS ISO 5305:2024"},"content":{"rendered":"
PDF Pages<\/th>\n | PDF Title<\/th>\n<\/tr>\n | ||||||
---|---|---|---|---|---|---|---|
2<\/td>\n | undefined <\/td>\n<\/tr>\n | ||||||
7<\/td>\n | Foreword <\/td>\n<\/tr>\n | ||||||
8<\/td>\n | Introduction <\/td>\n<\/tr>\n | ||||||
9<\/td>\n | 1 Scope 2 Normative reference documents 3 Terms and definitions <\/td>\n<\/tr>\n | ||||||
13<\/td>\n | 4 Abbreviated terms 5 Instrumentation 5.1 General 5.2 Calibration 6 General requirements 6.1 General <\/td>\n<\/tr>\n | ||||||
14<\/td>\n | 6.2 Requirements of acoustic far-field condition 6.3 Requirements of position of UAS to reduce aerodynamic flow effect 6.4 Requirements of position control 6.4.1 General 6.4.2 Requirement of position accuracy <\/td>\n<\/tr>\n | ||||||
15<\/td>\n | 6.4.3 Requirement of speed accuracy 6.5 Requirements of background noise 7 Anechoic chamber tests 7.1 General <\/td>\n<\/tr>\n | ||||||
16<\/td>\n | 7.2 Requirements of anechoic chamber 7.2.1 Size 7.2.2 Anechoic chamber qualification 7.3 Measurement configurations 7.3.1 General <\/td>\n<\/tr>\n | ||||||
18<\/td>\n | 7.3.2 Hover and yaw: 4-microphone approach <\/td>\n<\/tr>\n | ||||||
20<\/td>\n | 7.3.3 Hover and yaw: multiple microphone approach <\/td>\n<\/tr>\n | ||||||
21<\/td>\n | 7.3.4 Take-off and landing <\/td>\n<\/tr>\n | ||||||
23<\/td>\n | 7.3.5 Cruise flight <\/td>\n<\/tr>\n | ||||||
24<\/td>\n | 8 Anechoic wind tunnel tests 8.1 General 8.2 Requirements of anechoic wind tunnel 8.2.1 General 8.2.2 Wind tunnel test configurations <\/td>\n<\/tr>\n | ||||||
25<\/td>\n | 8.2.3 Refraction correction 8.2.4 Microphone clearance distance 8.2.5 Anechoic chamber size 8.3 Measurement configurations 8.3.1 General <\/td>\n<\/tr>\n | ||||||
26<\/td>\n | 8.3.2 Take-off and landing <\/td>\n<\/tr>\n | ||||||
28<\/td>\n | 8.3.3 Cruise flight <\/td>\n<\/tr>\n | ||||||
30<\/td>\n | 9 Outdoor tests 9.1 General <\/td>\n<\/tr>\n | ||||||
31<\/td>\n | 9.2 Recommendations of the test site <\/td>\n<\/tr>\n | ||||||
32<\/td>\n | 9.3 Recommendations and requirements of the meteorological conditions 9.4 Microphone configuration and layout 9.4.1 Microphone configuration 9.4.2 Microphone layout <\/td>\n<\/tr>\n | ||||||
33<\/td>\n | 9.5 Measurement corrections and limitations <\/td>\n<\/tr>\n | ||||||
34<\/td>\n | 9.6 Measurement procedures 9.6.1 General 9.6.2 Hover and yaw 9.6.3 Take-off and landing <\/td>\n<\/tr>\n | ||||||
35<\/td>\n | 9.6.4 Cruise flight 10 Uncertainties 10.1 General 10.2 Uncertainty sources and requirements <\/td>\n<\/tr>\n | ||||||
36<\/td>\n | 10.3 Evaluation of the uncertainty <\/td>\n<\/tr>\n | ||||||
37<\/td>\n | 11 Information to report 11.1 Test methods 11.2 Selected noise metrics 11.3 UAS under test 11.4 Test environment 11.5 Data acquisition system <\/td>\n<\/tr>\n | ||||||
38<\/td>\n | 11.6 Measurement 11.7 Results <\/td>\n<\/tr>\n | ||||||
39<\/td>\n | Annex A (Informative) Examples of the procedures to compute noise metrics from the recorded sound pressure signals <\/td>\n<\/tr>\n | ||||||
42<\/td>\n | Annex B (Informative) Numerical examination of the acoustic far-field condition <\/td>\n<\/tr>\n | ||||||
46<\/td>\n | Annex C (Informative) Measurement of far-field condition for a UAS propeller noise <\/td>\n<\/tr>\n | ||||||
48<\/td>\n | Annex D (Informative) An example of adjusting the UAS location to realize different equivalent observer angles <\/td>\n<\/tr>\n | ||||||
49<\/td>\n | Annex E (Informative) The effect of using windscreen for UAS propeller noise measurements <\/td>\n<\/tr>\n | ||||||
51<\/td>\n | Annex F (Informative) Examples of ground-board mounted microphone configurations <\/td>\n<\/tr>\n | ||||||
53<\/td>\n | Annex G (Informative) Uncertainty analysis example of a UAS noise measurement <\/td>\n<\/tr>\n | ||||||
56<\/td>\n | Bibliography <\/td>\n<\/tr>\n<\/table>\n","protected":false},"excerpt":{"rendered":" Noise measurements for UAS (unmanned aircraft systems)<\/b><\/p>\n |