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Last Updated: Jul 07, 2014
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ASTM F3002-14
Standard Specification for Design of the Command and Control System for Small Unmanned Aircraft Systems (sUAS)
Standard Specification for Design of the Command and Control System for Small Unmanned Aircraft Systems (sUAS)
F3002-14
ASTM|F3002-14|en-US
Standard Specification for Design of the Command and Control System for Small Unmanned Aircraft Systems (sUAS)
Standard
F3002 Standard Specification for Design of the Command and Control System for Small Unmanned Aircraft Systems (sUAS)>
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BOS Vol. 15.09 Committee F38
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Abstract
This specification provides a consensus standard for an application to a nation's governing aviation authority (GAA) for a permit to operate a small unmanned aircraft system (sUAS) for commercial or public use purposes. It is intended for all sUAS that are allowed to operate over a defined area and in airspace authorized by a nation's GAA. Unless otherwise specified by a nation's GAA, this specification applies only to UA that have a maximum gross takeoff weight of 25 kg (55 lb) or less. This specification covers general command and control (C2) requirements, C2 system spectrum requirements, C2 link requirements, UA requirements, and fly-away functionality.
Scope
1.1 This specification is provided as a consensus standard in support of an application to a nation’s governing aviation authority (GAA) for a permit to operate a small unmanned aircraft system (sUAS) for commercial or public use purposes.
1.2 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.