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TRANSCRIPT
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This may be the author’s version of a work that was submitted/acceptedfor publication in the following source:
Clothier, Reece A.(2012)Overview of Australian Civil UAS Regulations and Supporting Research.InThe Technical Cooperation Panel meeting AER (aerospace group), Tech-nical Panel 6 "UAV Systems and Operations", 2012-03-28 - 2012-03-28.(Unpublished)
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Overview of Australian Civil UAS Regulations and Supporting Research
Reece Clothier Senior Research Fellow
Australian Research Centre for Aerospace Automation Queensland University of Technology
28 March 2012
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Overview of Presentation
� Australian Civil UAS Context � Systems, operations and environment � Civil UAS regulations � Regulatory review
� ARCAA UAS Risk Research Program � Regulatory framework � Risk modelling � Safety objectives and social concerns
� ARCAA Enabling Technology Research Program � Australian led enabling research in flight termination systems,
Detect and Act, and automated separation management
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Australian Context – Industry & Systems
Kingfisher II BAE Systems Australia, VIC
ScanEagle Insitu Pacific Ltd, QLD
Flamingo – Silvertone, NSW CyberEye II – Cyber Technology, WA Medium Airship Airship Solutions, NSW
cyberQuad Cyber Technology, WA
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Aerosonde Mark 4.7 AAI, Aersonde VIC
Kestral Automated Target Detection Software,
Sentient, VIC CM160 Gimbaled
Camera UAV Vision, NSW
Phoenix Jet Aerial Targets Air Affairs Australia, NSW
T2000UAV-L, Mode 3/A Transponder Microair, QLD
i-Flight 650 Flight Vision, NSW
ARCAA Rotor-Wing UAS
ARCAA, QLD
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AirRobot Australasia, VIC
Australian Context – Industry & Systems
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Fire front mapping - WA 2010 – Photo: Channel 10
Insitu Pacific Ltd Marine Mammal Survey - Dugongs and Whale (Inset)
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Beach litter surveys, CSIRO. Photo: Tricia Watkinson.
Insitu Pacific Ltd- Fisheries protection & law enforcement trials. Photo: Channel 7
Australian Context – Civil Operations
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Insitu Pacific Fire and Emergency Services Trials 2009
Automated inspection of power lines. Photo taken from a UAS with automated power line
detection algorithm (ARCAA and CRC-SI)
� Current applications and demonstrations in: � Customs/border protection � Power-pole and communications
tower inspection � Aerial photography (e.g., real-estate) � Mine site rehabilitation � Noxious weed survey � Maritime poaching and fisheries
enforcement � Drug crop detection � Agriculture management � Search and rescue � Surf life saving
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Australian Context – Civil Operations
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� Extremely low population density � 95% of Australia by land area has density < 1 person km2
� Airspace and Air Traffic Services � Low aircraft activity away from populated centres and eastern air
routes � Huge amount of Class G/uncontrolled airspace (99.88% of FIR):
� SFC to ~8,500ft / FL180 (Radar/Non-radar) � Class G in the US NAS: SFC to 1,200ft AGL
� PSR and SSR coverage limited to eastern coast and major populated centres
� ADS-B mandatory equipage: � New aircraft from Feb 2014 for operation in airspace Classes A, B, C
and E and above 10,000 feet in Class G; and � By Feb 2016 for ALL aircraft operating at Melbourne, Sydney,
Brisbane and Perth Airports (Class C). � ALL existing and new IFR capable aircraft (by 2017 / from 2014) � Class A operations > FL290
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Australian Context – Operating Environment
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8 PSR, SSR and ADS-B end state coverage 5,000ft AGL PSR, SSR and ADS-B end state coverage 10,000ft AGL PSR, SSR and ADS-B end state coverage FL200 PSR, SSR and ADS-B end state coverage FL300
Coverage pictures compliments of Airservices Australia
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Australian Context - Civil UAS Regulations
� CASA was first in the world to define civil regulations for UAS, 2002
� Operational regulations contained in CASR 1998, Part 101
� Three operational categories defined � MICRO ≤ 100g � 100g < SMALL ≤ 150 kg (100 kg rotorcraft) � LARGE > 150kg (100 kg rotorcraft)
� Operations approved on a case-by-case basis � Within an “approved area” or in accordance with conditions associated with
the operator’s OC � Restrictions depend on safety case, can include:
� Limited to VLOS, defined area, altitude, not over populous areas
� Additional requirements on personnel, equipage, communication and planning � Letter of agreement with Air Service Provider
� Commercial operations require operator to obtain an OC
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� Certificate of Airworthiness required for: � All large UAS operations � All small and large UAS operations over “populous areas”
� No type certification standards have been defined: � Experimental designation - AC 21-43(0)
� specific applications and not for commercial reward, subject to operational restrictions.
� Certification as a restricted category � No standards or guidance provided – assessed individually
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Australian Context - Civil UAS Regulations
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Regulatory Reform � Current regulations have greatly benefited civil industry
� Industry grown to a point where further guidance is needed to permit greater freedom of operations, consistent regulation across sectors and harmonisation to international initiatives
� “Grey areas” in current regulation
� April 2009 Australia Aerospace Industry Forum, Certification & Regulation Working Group for UAS was formed � Made recommendations to CASA on certification framework, training and
licensing, operations in class G airspace, and definition of populous areas [REF 1]
� The Aviation White Paper (released December 2009 and available on The Department of Infrastructure and Transport Website) stated that the Government will ensure CASA “…enhances oversight of the operation of unmanned aerial vehicles (UAVs)”
� June 2011 – CASA Project OS 11/20 established to review CASR 101 and ACs
� Nov 2011 – CASA Standards Consultative Committee Working Group formed to assist with Project OS 11/20
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Regulatory Reform
� Revision of Advisory Circulars underway (released for public consultation ~ June 2012) � Release includes significant input from DGTA, ACPA, DSTO, UAS
industry, academia, other airspace user groups
� Will include: � New personnel training and licensing requirements � New requirements on Operator Certification and area approvals � Emphasis on safety outcome-based regulation as opposed to
prescriptive codes of requirements
� CASA Direction - Target system safety approach � The minimum requirements and guidance material on the
preparation of operational safety cases are being developed � Acknowledged that some larger UAS operations may be type
certificated in the future – not for some time
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ARCAA – Supporting Civil UAS Regulatory Reform
Risk-informed regulation of civil UAS
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ARCAA Risk-Based Regulatory Framework
� ARCAA, in conjunction with researchers from DSTO and CSIRO proposed a risk-based structuring of civil regulations for UAS [REF 1, 2]
� Framework was endorsed by Australian industry (AAIF) and by CASA as an appropriate framework for the development of regulatory requirements on civil UAS: � Technical airworthiness � UAS operations within non-segregated airspace
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Risk-Based Framework
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Defined by the degree of harm a UAS could cause to an area over-flown. Note: the type categories are defined independent of the particular area over-flown (orthogonal to the axis describing the operational environment)
UAS Types
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Defined by the potential for harm given a UAS crashing in the area (characterised by the susceptibility of an area to a crashing UAS: population density, degree of sheltering, hazardous industry etc). Note: the categories of operational environment are defined independent of the particular type of UAS over-flying (orthogonal to the type category axis)
UAS Operational Environment
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Each cell of the matrix defines a unique operational scenario - the combination of a UAS type and particular operating environment
UAS Operational Scenarios
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The level of risk is determined for each cell (operational scenario).
Risk Assessment
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Cells of a similar colour represent a similar level of risk and hence are subject to the same airworthiness requirements.
The spectrum of risk is then ‘mapped’ to a finite and contiguous number of UAS certification categories (r). Illustratively, this is the process of assigning a finite number of colours to the cells.
UAS Certification Categories
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Risk-Based Framework
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Incorporating Airspace Integration
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Summary � Framework provides:
� Transparent and justifiable basis for tailoring requirements on UAS (design, manufacture, maintenance, training and licensing, and operation) across the diversity of systems, account for differences in: levels of risk, public acceptability and technical and performance constraints/limitations
� Systematic treatment of technical and operational mitigation strategies � Consistent with ICAO SARPS mandating NAA activities of policy, rulemaking
and oversight be risk based
� Does not prescribe how regulation is promulgated: � Prescriptive code of requirements or � Outcome based safety case
� Concept endorsed by CASA [REF 3] as the preferred framework for: � Establishing technical airworthiness requirements � Generating and evaluating safety cases for UAS operations in non-segregated
airspace and over inhabited areas
� Research project has been established to substantiate framework � Recommendations to CASA via AAIF expected by June 2014
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Risk Modelling � Key component is QRA of UAS operations in non-segregated
airspace and over inhabited areas
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� Primary focus to date has been the modelling of ground risk [REF 4] � Detailed and high-level ground risk
quantified assessment tools
� Impact footprint modelling
� Modelling of aircraft failure modes
� Establishing system-level safety objectives for UAS
� Developed QRA Tool for DSTO – high level assessments of ground risk [REF 5]
� New work to develop a systems theoretic communication risk model for generic UAS operations in Australian non-segregated airspace
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Risk-based Classification of UAS Types
� The specification of the “Columns” of the risk framework
� Preliminary studies with DSTO into risk-based classification of UAS types [REFS 6, 7]
� Established funded research project to determine: � Harm of micro/small
UAS (Dec 12) � Finalisation of risk-
based type categories(June 13)
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Classification by Individual Risk
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X-‐45C
RQ-‐11A/B Raven
FQM-‐151A Pointer
Brumby, Mk3
Black Widow Wasp II
RQ-‐14A Dragon Eye KillerBee 2
Aerosonde Mk 4 ScanEagle
RQ-‐7A, Shadow 200
RQ-‐2A/B Pioneer
I-‐View 250
Shadow 600
Sky Lark IV
Helios
MQ-‐5C e-‐Hunter
M/RQ-‐1B Predator
Heron 1
MQ-‐12A Sky Warrior
RQ-‐3A DarkStar
Taranis
RQ-‐4B Global Hawk
RQ-‐37A
MQ-‐9B Reaper
Centurion
CL-‐89_Midge
Scarab
Sky-‐X Eagle Eye
Mobius 4
Log10 Impact Energy (J)
Log 1
0 Impact Area (m
2 )
Type category 1 Type category 2 Type category 3 Type category 4 Type category 5
Candidate type categories for fixed-‐wing UAS
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Safety Objectives and Public Concern
� Preliminary work in the quantified specification of high level safety objectives (i.e., the equivalent level of safety objective) [REF 8]
� Research program established and funded to: � Review and finalisation of a set of quantified safety objectives for UAS
(Dec 2012)
� Extensive stakeholder survey to: � Identify public concerns (June 2014)
� Quantify public attitude towards risks (June 2014)
� Develop stakeholder communication strategies (June 2014)
� Recommendations to be made to CASA via the AAIF
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Addressing the Technical Challenges…
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Automated Emergency Landing Systems
Safe landing of aircraft
High altitude continuous mapping.
High level landing site identification
Site selection, dynamic path planning, guidance and control down to final decision point
Low altitude site characterisation, dynamic path planning, guidance and control.
Engine Failure
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Research – Automated Emergency Landing System Algorithm Developed by
D.L Fitzgerald
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Automated Midair Collision Avoidance System
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Global Assurance
Local Assurance
4. Automated Separa�on Management System
1.
2.
3.
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Smart Skies – Flight Demonstrated Technologies
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Smart Skies – ASMS � Automated separation provision for complex airspace
management scenarios [REF 9]
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� Automated control of real flight test aircraft for separation assurance using public data networks and Iridium
� Real world scenarios � Up to 50 real & sim AC � Mix of types and
performance � Non-coop and active
breakdown scenarios � Rotorcraft
� Incorporated PSR and ADS-B surveillance feeds and aircraft-based separation (Detect and Act)
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Real World Flight Test Results
Complex scenarios: C172 Primary Flight Display showing some of the 49 other aircraft
UAS on UAS Scenarios
UAS on C172 Scenarios
Scenarios using radar data
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Summary � Australian civil regulations are progressing rapidly after more
than a decade of stagnation
� CASA general direction is towards safety target based regulation
� A large number of technical and social (regulatory and public concern) issues still need to be addressed
� Integrated program of research has been established by ARCAA � Risk studies underpinning substantiation of a risk-based
framework for the regulation of UAS operations over inhabited areas and in non-segregated airspace
� Output are recommendations to the regulator via independent industry group (AAIF or CASA SCC)
� Ongoing development and flight testing of existing risk mitigation technologies � Detect and Act � Automated Flight Emergency Landing System
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References
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[1] Recommendations Of the Australian Aerospace Industry Forum Sub-Committee on UAS Certification and Regulation for Routine Access of Small UAS to Class G Airspace (Nov 2010). Download: http://www.innovation.gov.au/Industry/Aerospace/Forum/Documents/AAIF_%20UAS_%20Report.pdf
[2] Clothier, Reece A., Palmer, Jennifer L., Walker, Rodney A., and Fulton, Neale L. (2011) Definition of an airworthiness certification framework for civil unmanned aircraft systems. Safety Science. Vol. 49 (6), July. pp. 871-885. Author version download: http://eprints.qut.edu.au/40466/
[3] “CASA Response to Unmanned Aircraft Systems Sub-committee Report”, Letter from T Farquharson (A/g Director of Aviation Safety, CASA) to AAIF Chair, Mr Ian Honnery (Dated 12 May 2011)
[4] Clothier, Reece A., Walker, Rodney A., Fulton, Neale, & Campbell, Duncan A. (2007) A Casualty Risk Analysis For Unmanned Aerial System (UAS) Operations Over Inhabited Areas. In AIAC12 – Twelfth Australian International Aerospace Congress, 2nd Australasian Unmanned Air Vehicles Conference, 19-22 March, Melbourne. Author version download: http://eprints.qut.edu.au/6822/
[5] Wu, P and Clothier R. ARCAA-URAT-RM-MD-001, UAS Risk Assessment Tool Project: Risk Model Derivation. Technical Report to Defence Science and Technology Organisation (DSTO). Australian Research Centre for Aerospace Automation (ARCAA), Brisbane, Australia. 14 April 2011
[6] Clothier, Reece A., Palmer, Jennifer L., Walker, Rodney A., and Fulton, Neale L. (2010) Definition of airworthiness categories for civil Unmanned Aircraft Systems (UAS). In Proceedings of The 27th International Congress of the Aeronautical Sciences, Acropolis Conference Centre, Nice, France. Author version download: http://eprints.qut.edu.au/32789/
[7] Clothier, Reece A. (2011) UAS Classification: Key to effective airworthiness and operational regulations. In Royal Aeronautical Society Unmanned Aircraft Systems Specialist Group, UAS Classification Workshop, 24th June 2011, London, UK. (Unpublished). Author version download: http://eprints.qut.edu.au/42054/
[8] Clothier, Reece A. & Walker, Rodney A. (2006) Determination and Evaluation of UAV Safety Objectives. In 21st International Unmanned Air Vehicle Systems Conference, 3rd April - 5th April 2006, Bristol, United Kingdom. Author version download: http://eprints.qut.edu.au/4183/
[9] Clothier, Reece A., Frousheger, D. and Wilson, M. (2012) The Smart Skies Project: ICAS 2012. Submitted for presentation at The 28th International Congress of the Aeronautical Sciences, Brisbane, Australia (to appear).
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QUESTIONS
Reece Clothier
Australian Research Centre for Aerospace Automation
www.arcaa.aero
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More Information
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C172 Flight Display
Experiment View
Simple Initial Collision Scenarios