Unmanned aircraft systems — Part 2: UAS components

This document specifies requirements for ensuring the quality and safety of the design and manufacture of unmanned aircraft systems (UAS) that include unmanned aircraft (UA), remote pilot stations (RPS), datalinks, payloads, and associated support equipment. This document includes information regarding the unmanned aircraft, any associated remote pilot station (RPS)(s), the command and control links (C2 Link), any other required data links (e.g. payload, traffic management information, vehicle identification) and any other system elements as can be required. This document does not cover passenger carrying UAS or technical requirements for the design and manufacturing for UAS components. This document does not include equipment considerations unique to compliance with UA traffic management systems. The document is applicable to the reasonable expected use of a UAS. This document is applicable: a) to UAS designed for use where a State aviation authority has determined a Certificate of Airworthiness (C of A) is not required; b) where a C of A is required, to complement technical standards published by the aviation authority for the purposes of building the certification basis; or c) as an alternative means of compliance if acceptable to the aviation authority.

Aéronefs sans pilote — Partie 2: Composants des UAS

General Information

Status
Published
Publication Date
09-Dec-2021
Current Stage
6060 - International Standard published
Start Date
10-Dec-2021
Due Date
05-Dec-2021
Completion Date
10-Dec-2021
Ref Project
Standard
ISO 21384-2:2021 - Unmanned aircraft systems
English language
38 pages
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Standards Content (Sample)


INTERNATIONAL ISO
STANDARD 21384-2
First edition
2021-12
Unmanned aircraft systems —
Part 2:
UAS components
Aéronefs sans pilote —
Partie 2: Composants des UAS
Reference number
© ISO 2021
All rights reserved. Unless otherwise specified, or required in the context of its implementation, no part of this publication may
be reproduced or utilized otherwise in any form or by any means, electronic or mechanical, including photocopying, or posting on
the internet or an intranet, without prior written permission. Permission can be requested from either ISO at the address below
or ISO’s member body in the country of the requester.
ISO copyright office
CP 401 • Ch. de Blandonnet 8
CH-1214 Vernier, Geneva
Phone: +41 22 749 01 11
Email: copyright@iso.org
Website: www.iso.org
Published in Switzerland
ii
Contents Page
Foreword .vii
Introduction .viii
1 Scope . 1
2 Normative references . 1
3 Terms and definitions . 1
4 Abbreviated terms . 2
5 General design requirements for UAS. 4
5.1 General . 4
5.2 Function and reliability . 4
5.2.1 Design . 4
5.2.2 Components . 5
5.3 Maintainability and supportability . 5
5.3.1 Design . 5
5.3.2 Documentation. 5
5.3.3 Support . 6
5.4 Fatigue durability . 6
5.5 Aircraft identification features . 6
5.6 Transportation, storage and packaging . 6
6 Aircraft structures . 7
6.1 Overview . 7
6.2 Damage tolerance assessment . 7
6.3 UA construction . 7
6.4 Moving parts . 8
6.5 Attached parts . 8
7 Propulsion . 8
7.1 Propulsion risk management . 8
7.2 Engines and motors . . 8
7.2.1 General requirements . 8
7.2.2 Mounting and installation . 8
7.2.3 Combustion engines . 9
7.2.4 Electric motors . 9
7.2.5 Electronic speed controller (ESC) requirements . 9
7.3 Thrust mechanisms . 9
7.3.1 Propellers and rotors . 9
7.3.2 Turbine and fans . 10
8 Electrical systems .10
8.1 General . 10
8.2 Electrical safety . 10
8.3 Airborne electrical systems . 10
8.4 Ground electrical systems . 10
8.4.1 UAS electrical components on the ground . 10
8.4.2 RPS power system . 11
8.4.3 Labelling . 11
9 Energy sources .11
9.1 Batteries . 11
9.1.1 General . 11
9.1.2 Protective measures . 11
9.1.3 Precautions . 11
9.2 Combustible fuels . 11
9.3 Fuel cells .12
9.3.1 General requirements .12
iii
9.3.2 General safety requirements .12
9.3.3 Protective measures .12
10 Equipment .12
10.1 Avionic equipment (general). 12
10.2 Flight control system (FCS) . 13
10.2.1 General requirement . .13
10.2.2 Flight control hardware .13
10.2.3 Flight control software . 14
10.2.4 Course accuracy . 14
10.2.5 Airspeed . 14
10.3 Flight control actuators .15
10.4 Diagnostics . 15
10.5 Navigation systems . 15
10.5.1 General .15
10.5.2 Global Navigation Satellite System (GNSS) receiver . 15
10.5.3 Real time kinematic (RTK) augmentation. 15
10.5.4 Inertial measurement unit (IMU) . 16
10.5.5 Magnetic compass . 16
10.6 Attitude sensors . 16
10.6.1 Altimeter . 16
10.6.2 Airspeed sensor.
...

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