{"id":423318,"date":"2024-10-20T06:45:51","date_gmt":"2024-10-20T06:45:51","guid":{"rendered":"https:\/\/pdfstandards.shop\/product\/uncategorized\/bsi-23-30426803-dc-2023\/"},"modified":"2024-10-26T12:41:24","modified_gmt":"2024-10-26T12:41:24","slug":"bsi-23-30426803-dc-2023","status":"publish","type":"product","link":"https:\/\/pdfstandards.shop\/product\/publishers\/bsi\/bsi-23-30426803-dc-2023\/","title":{"rendered":"BSI 23\/30426803 DC 2023"},"content":{"rendered":"
PDF Pages<\/th>\n | PDF Title<\/th>\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 <\/td>\n<\/tr>\n | ||||||
10<\/td>\n | 3 Terms and definitions <\/td>\n<\/tr>\n | ||||||
13<\/td>\n | 4 List of abbreviated terms 5 Instrumentation 5.1 General 5.2 Calibration <\/td>\n<\/tr>\n | ||||||
14<\/td>\n | 6 General requirements 6.1 General 6.2 Requirements of acoustic far-field condition 6.3 Requirements of position of UAS to reduce aerodynamic flow effect <\/td>\n<\/tr>\n | ||||||
15<\/td>\n | 6.4 Requirements of position control 6.4.1 Requirement of position accuracy 6.4.2 Requirement of velocity accuracy 6.5 Requirements of background noise <\/td>\n<\/tr>\n | ||||||
16<\/td>\n | 7 Anechoic chamber tests 7.1 General 7.2 Requirements of anechoic chamber 7.2.1 Size 7.2.2 Anechoic chamber qualification <\/td>\n<\/tr>\n | ||||||
17<\/td>\n | 7.3 Measurement configurations <\/td>\n<\/tr>\n | ||||||
18<\/td>\n | 7.3.1 Hover and yaw: 4-microphone approach <\/td>\n<\/tr>\n | ||||||
19<\/td>\n | 7.3.2 Hover and yaw: multiple microphone approach <\/td>\n<\/tr>\n | ||||||
21<\/td>\n | 7.3.3 Take-off and landing <\/td>\n<\/tr>\n | ||||||
22<\/td>\n | 7.3.4 Cruise flight <\/td>\n<\/tr>\n | ||||||
23<\/td>\n | 8 Anechoic wind tunnel tests 8.1 General <\/td>\n<\/tr>\n | ||||||
24<\/td>\n | 8.2 Requirements of anechoic wind tunnel 8.2.1 Wind tunnel test configurations 8.2.2 Refraction correction 8.2.3 Microphone clearance distance 8.2.4 Anechoic chamber size 8.3 Measurement configurations <\/td>\n<\/tr>\n | ||||||
25<\/td>\n | 8.3.1 Take-off and landing <\/td>\n<\/tr>\n | ||||||
26<\/td>\n | 8.3.2 Cruise flight <\/td>\n<\/tr>\n | ||||||
28<\/td>\n | 9 Outdoor tests 9.1 General <\/td>\n<\/tr>\n | ||||||
29<\/td>\n | 9.2 Recommendations of the test site 9.3 Recommendations of the meteorological conditions <\/td>\n<\/tr>\n | ||||||
30<\/td>\n | 9.4 Microphone configuration and layout 9.4.1 Microphone configuration 9.4.2 Microphone layout <\/td>\n<\/tr>\n | ||||||
31<\/td>\n | 9.5 Measurement corrections and limitations 9.6 Measurement procedures <\/td>\n<\/tr>\n | ||||||
32<\/td>\n | 9.6.1 Hover and yaw 9.6.2 Take-off and landing 9.6.3 Cruise flight <\/td>\n<\/tr>\n | ||||||
33<\/td>\n | 10 Uncertainties 10.1 General 10.2 Uncertainty sources and requirements 10.3 Evaluation of the uncertainty <\/td>\n<\/tr>\n | ||||||
34<\/td>\n | 11 Information to report 11.1 Test methods 11.2 Selected noise metrics 11.3 UAS under test <\/td>\n<\/tr>\n | ||||||
35<\/td>\n | 11.4 Test environment 11.5 Data acquisition system 11.6 Measurement 11.7 Results <\/td>\n<\/tr>\n | ||||||
37<\/td>\n | Annex\u20acA (Informative) Examples of the procedures to compute noise metrics from the recorded sound pressure signals <\/td>\n<\/tr>\n | ||||||
40<\/td>\n | Annex\u20acB (Informative) Numerical examination of the acoustic far-field condition <\/td>\n<\/tr>\n | ||||||
43<\/td>\n | Annex\u20acC (Informative) Measurement of far-field condition for a UAS propeller noise <\/td>\n<\/tr>\n | ||||||
45<\/td>\n | Annex\u20acD (Informative) An example of adjusting the UAS location to realize different equivalent observer angles <\/td>\n<\/tr>\n | ||||||
46<\/td>\n | Annex\u20acE (Informative) The effect of using windscreen for UAS propeller noise measurements <\/td>\n<\/tr>\n | ||||||
47<\/td>\n | Annex\u20acF (Informative) Examples of ground-board mounted microphone configurations <\/td>\n<\/tr>\n | ||||||
49<\/td>\n | Annex\u20acG (Informative) Uncertainty analysis example of a UAS noise measurement <\/td>\n<\/tr>\n | ||||||
51<\/td>\n | Bibliography <\/td>\n<\/tr>\n<\/table>\n","protected":false},"excerpt":{"rendered":" BS ISO 5305. Noise measurements for UAS (Unmanned aircraft systems)<\/b><\/p>\n |