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BS ISO 21384-2:2022

BS ISO 21384-2:2022

$189.07

Unmanned aircraft systems – UAS components

Published By Publication Date Number of Pages
BSI 2022 50
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PDF Catalog

PDF Pages PDF Title
2 National foreword
9 Foreword
10 Introduction
11 1 Scope
2 Normative references
3 Terms and definitions
12 4 Abbreviated terms
14 5 General design requirements for UAS
5.1 General
5.2 Function and reliability
5.2.1 Design
15 5.2.2 Components
5.3 Maintainability and supportability
5.3.1 Design
5.3.2 Documentation
16 5.3.3 Support
5.4 Fatigue durability
5.5 Aircraft identification features
5.6 Transportation, storage and packaging
17 6 Aircraft structures
6.1 Overview
6.2 Damage tolerance assessment
6.3 UA construction
6.4 Moving parts
18 6.5 Attached parts
7 Propulsion
7.1 Propulsion risk management
7.2 Engines and motors
7.2.1 General requirements
7.2.2 Mounting and installation
19 7.2.3 Combustion engines
7.2.4 Electric motors
7.2.5 Electronic speed controller (ESC) requirements
7.3 Thrust mechanisms
7.3.1 Propellers and rotors
20 7.3.2 Turbine and fans
8 Electrical systems
8.1 General
8.2 Electrical safety
8.3 Airborne electrical systems
8.4 Ground electrical systems
8.4.1 UAS electrical components on the ground
8.4.2 RPS power system
21 8.4.3 Labelling
9 Energy sources
9.1 Batteries
9.1.1 General
9.1.2 Protective measures
9.1.3 Precautions
9.2 Combustible fuels
9.3 Fuel cells
9.3.1 General requirements
22 9.3.2 General safety requirements
9.3.3 Protective measures
10 Equipment
10.1 Avionic equipment (general)
23 10.2 Flight control system (FCS)
10.2.1 General requirement
10.2.2 Flight control hardware
10.2.3 Flight control software
24 10.2.4 Course accuracy
10.2.5 Airspeed
10.3 Flight control actuators
25 10.4 Diagnostics
10.5 Navigation systems
10.5.1 General
10.5.2 Global Navigation Satellite System (GNSS) receiver
10.5.3 Real time kinematic (RTK) augmentation
10.5.4 Inertial measurement unit (IMU)
26 10.5.5 Magnetic compass
10.6 Attitude sensors
10.6.1 Altimeter
10.6.2 Airspeed sensor
27 10.6.3 Optical sensor
10.7 Hardware and software redundancy
10.8 Failure modes
28 11 C2 Link
11.1 Performance and design
11.2 Antenna module design
11.3 Operations
11.4 Monitoring
29 11.5 Protocol
11.6 Data features
11.6.1 General
11.6.2 UA status data
11.6.3 Delay requirements
11.7 Reliability requirements
11.8 Security requirements
30 12 Remote pilot station
12.1 General
12.2 Features
12.2.1 General
12.2.2 Data monitoring systems requirements
12.3 Design requirements
12.3.1 System
12.3.2 Structure
31 12.3.3 Human factors engineering and ergonomics design
12.4 Functional requirements
12.4.1 Mission planning
12.4.2 Data link control
12.4.3 Flight Control Commands
12.5 Displays
12.5.1 Instrumentation
32 12.5.2 Readability
12.5.3 Accuracy
12.5.4 Warnings, cautions, and advisories
12.5.5 Display/interface failures
12.5.6 Track and parameter display
33 12.5.7 C2 Link status display
12.5.8 Telemetry parameter record
12.6 Performance requirements
12.6.1 Environmental adaptability
12.6.2 Reliability
34 12.7 Safety
12.8 Collision avoidance (CA) systems
13 Payload
13.1 General requirements
13.2 Safety marking
35 13.3 Wiring design
13.4 Payload power supply
13.5 Storage requirement
14 Airworthiness
14.1 Documentation
14.1.1 Instructions
14.1.2 Manuals and handbooks
14.1.3 Procedural changes
14.2 Composition of an operator’s manual
14.2.1 Technical specifications
36 14.2.2 Flight performance
14.2.3 Aircraft weights
14.2.4 Flight control accuracy
14.2.5 Dimensions
14.2.6 Atmospheric and other environments adaptability
37 14.3 Electromagnetic compatibility considerations
14.4 Noise
14.5 Built-in test and monitoring
14.6 System safety program
14.6.1 Selection of design materials
38 14.6.2 Properties and processes
14.6.3 Mass properties
14.6.4 Corrosion
39 14.6.5 Material limitations
14.6.6 Fire hazards
14.6.7 Equipment separation
15 UAS software
15.1 Software architecture and design
15.2 Safety
40 15.3 Security
15.4 Software compliance
15.5 Software development life cycle
16 Other considerations
16.1 Ground equipment
16.2 Multi vehicle control
41 16.3 Jamming and spoofing
17 Automation
17.1 General
17.2 Software development lifecycle
17.3 Remote pilot intervention
17.4 System data collection
17.5 Automation risk assessment
42 17.6 Automation system architecture
43 Annex A (informative) Software risk management
46 Annex B (informative) Electromagnetic environmental effects (E3)
48 Bibliography

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BS ISO 21384-2:2022
$189.07