UAV Certification - extract for AUVSI 2015
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Transcript of UAV Certification - extract for AUVSI 2015
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UAV Certification
Recognised Certification Bases
Regulation – An Australian Perspective
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Overview
Regulation and Certification
Manned vs unmanned regulation
Unmanned aviation regulation
UAS Certification Bases
Pros and cons of manned certification bases
Scope of UAS certification
Fundamentals of UAS certification
Standards
MIL-HDBK-516B, STANAG 4671
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Regulation and Certification
What is regulation?
The framework
What is a certification basis?
The set of requirements that define the airworthiness standards to which an aircraft is designed / built
Why is UAS certification different?
Often unable to meet manned criteria
Different risk profiles
Becomes risk-oriented
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Regulation
Consistently regulated across the globe
International Civil Aviation Organisation
ICAO
Framework for regulation of (civil) aviation
Manned
National and Military Airworthiness Authorities
Well recognised standards and mutual recognition
Unmanned
Widely varying regulation worldwide
No universally accepted standards
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Fundamental Certification Aspects
Why use a manned certification basis?
Recognised by airworthiness authorities
Understood by engineers
Commonalities: UAVs & manned aircraft
Maintenance / Reliability
Structural integrity
EMI/EMC (but more critical in UAS)
Fatigue and life management
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Fundamental Certification Aspects
Why not use a manned certification basis?“Too safe” for unmanned aircraft?
Omits critical UAS-specific aspects
Inappropriate for UAS size and development history
Differences: UAVs vs manned aircraftLoss of aircraft ≠ Loss of pilot
Lower weight, larger wingspan than manned
Ability to terminate flight
Limited on-board sense and avoid capability
100% electrical system (no manual override)
Engine (rather than pilot) likely single point of failure
Criticality of navigation system
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Airworthiness StandardsPhysical
MIL-HDBK-516BGuidance, not requirements
STANAG 4671 Tailored FAR23
DEF STAN 00-970 Part 9Tailored STANAG 4671
CS-LURSTailored FAR27 (Rotorcraft)
UAV-GCS InterfaceSTANAG 4586
SoftwareDO-178B – not UAS-unique
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MIL-HDBK-516B"This document establishes the airworthiness certification criteria to be used in the determination of airworthiness of all manned and unmanned, fixed and rotary wing air vehicle systems. It is a foundational document to be used by the system program manager, chief engineer, and contractors to define their air system’s airworthiness certification basis.
Consists of:
Certification criteria
E.g. “Verify that the stability and control effects of basic design features, as well as unique features, are safe in the entire flight envelope(s).“
Recommended standards
14CFR references: 23.321-23.459, 25.321-25.459, 23.1501-23.1529, 25.1501-25.1529
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MIL-HDBK-516B
Theoretically includes unmanned aircraft
Limited specific coverage
Does not include GCS
Development of a certification basis
Airworthiness certification framework
Not a certification basis (CBD) in itself
Guides selection of standards, requirement thresholds, certification philosophy
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STANAG 4671“This document contains a set of technical airworthiness requirements intended primarily for the airworthiness certification of fixed-wing military UAV Systems with a maximum take-off weight between 150 and 20,000 kg (330 lb to 44,000 lb) that intend to regularly operate in non-segregated airspace.”
Based on 14 CFR Part 23 (FAR 23)
Excludes elements not relevant to UAS
Aerobatics, control forces, dual controls etc.
Adds UAS-unique elements
GCS, Flight Termination System etc.
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STANAG 4671
Manned-common elements
Generally match FAR 23 requirements
Some changes in thresholds
Change from pilot-oriented to FCS-oriented
Structure, engine etc
USAR.xxx
UAS-unique elements (approx 120)
Parachute systems
Launch systems
Flight termination systems
Communication systems
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...
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Summary
Certification is intended to ensure safety
Covers the entire system
UAV, GCS, pilots, maintainers
UAS certification is immature compared to manned aircraft certification
Same concepts apply
Lack of widely accepted standards
Existing standards are a solid baseline
Risk assessment is key to UAS operations
Air traffic integration aspects
Watch this (air)space
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Questions?
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