Safety and Security Driven Design. Unmanned Aircraft-National Airspace System Integration Case Study



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2 nd uropean STAMP Workshop, 2014 Safety and Security Driven Design. Unmanned Aircraft-National Airspace System Integration Case Study Kip Johnson Prof. Nancy eveson See accompanying abstract: Johnson, K., eveson, N. Investigating Safety and Cybersecurity Design Tradespace for Manned- Unmanned Aerial Systems Integration Using Systems Theoretic Process Analysis. in Proceedings of the Gesellschaft für Informatik, 2014. 23 Sept, 2014 Presentation approved for public release. 1

Disclaimer This work is sponsored by the Department of the Air Force under Air Force Contract #FA8721-05-C- 0002. The views expressed in this presentation are those of the authors and do not reflect the official policy or position of the United States Air Force, Department of Defense, or the U.S. Government. Presentation approved for public release. Case 88ABW-2014-4381 2

Overview Introduction Background Application of STAMP-STPA Conclusions 3

Introduction Problem Statement. How to assess and design Unmanned Aircraft System (UAS) integration into the National Airspace System (NAS)? Safety and (cyber) security are critical to system What is the design space for safety and security? What is the Human-Automation ontology necessary for safe and secure flight operations? 2014, Kip Johnson, All ights eserved 4

Introduction Motivation. eal world. Today, laborious accommodation of unmanned aerial systems (UAS) within the National Airspace System (NAS), or use in isolated military operations 545 UAS Certificate of Authorizations, Dec 13 [1] xponential UAS use in DoD past decade -> ecent Projections [2] Teal Group (2013). esearch & Development / Procurement $5.2-$11.6B annually next decade Future, seamless UAS integration into manned operations. FAA on UAS-NAS integration [4] Figure 1. DoD UAS Flight Hour Summary [3] Fig. 1. DoD UAS Flight Hour Summary. Fig. 1 adapted from [3] Ultimately, UAS must be integrated into the NAS without reducing existing capacity, decreasing safety, negatively impacting current operators, or increasing the risk to airspace users or persons and property on the ground 5 2014, Kip Johnson, All ights eserved

Introduction Motivation. Intellectual. Systems Theory applied to Systems ngineering (S) UAS Integration is a Complex Sociotechnical System Safety and Security are emergent properties; framed and analyzed as a control problem. eveson and Young [6] Application of S to UAS integration STAMP-STPA, and Safety and Security Driven Design Iterative relationship. Assess Design Most benefit in conceptual design and requirements generation Aids in comprehension of system complexity Fig. 2. Systems ngineering. Fig. 2 adapted from Defense Acquisition Guidebook, Chpt 4 [7] 2014, Kip Johnson, All ights eserved 6

Introduction Hypothesis: A systems-theoretic process analysis can be applied to the design and evaluation of safe and cyber-secure integrated manned-unmanned aerial system operations. A coupled safety and cybersecurity S assessment will demonstrate system design and evaluation benefits over independent analyses. UAS automation ontology for safe and secure integrated operations can be derived from S analyses. Method. Systems engineering approach Adaptation of Systems Theoretic Accident Model and Processes for system hazard and vulnerability analyses. 2014, Kip Johnson, All ights eserved 7

Overview Introduction Background Application of STAMP-STPA Conclusions 8

Background UAS-NAS Integration. Challenging Problem International efforts Began in the 1990s International Civil Aviation Organization US efforts Vision 100 Century of Aviation eauthorization Act (NextGen), 2003 Congress mandated FAA to accommodate UAS operations. 2012, FAA Modernization & eform Act Small UAS rule by Sep 2014 UAS integration into the NAS, Sep 2015 uropean fforts uropean Organization for Civil Aviation quipment (UOCA) Current efforts. adio Technical Committee for Aeronautics TCA Steering Committee- 228 to develop performance standards for key UAS technologies Detect and Avoid (DAA) Communications and Control (C2) Safety Assessment key effort for the NAS-level change 2014, Kip Johnson, All ights eserved 9

Background Current safety assessment efforts [8][9] Goal. Integration does not decrease safety Accident of interest. Mid-air collisions (MAC) System safety metric. Target level of safety, collision rate (λ). e.g. 1x10-9 MAC/hr Detect and Avoid safety metric. isk ratio of λ. λ mitigated / λ unmitigated, Mitigated = λ w/ Detect & Avoid System Many efforts-human factors studies, model and simulation (M&S), etc.-feed these quantitative safety assessments Traditional methods used, such as Bow-Tie model, fault and event trees. 2014, Kip Johnson, All ights eserved 10

Background Current safety barrier paradigm Air traffic control perspective US airspace does not completely match (dotted oval) UAS-NAS integration ose See & Avoid What about C2? Fig 3. NAS Barriers to Collision 2014, Kip Johnson, All ights eserved 11

Overview Introduction Background Application of STAMP-STPA Conclusions 12

Application of STAMP-STPA System of interest. Manned-Unmanned integrated flight operations High level system safety control structure System goal. Safe and secure integration Objectives. No new hazards from introduction of UAS remote operations Accidents of interest. Mid-air collision Ground collision (not a focus) H1 H2 H3 INTGATION SYSTM HAZAD System control actions lead to loss of aircraft minimum separation standards System control actions induce or contribute to a controlled flight into terrain maneuver System control actions induce or contribute to loss of aircraft controlled flight Fig 4. UAS Integration Safety Control Structure 2014, Kip Johnson, All ights eserved 13

Application of STAMP-STPA Major assumptions Manufacturing, certification, airworthiness, maintenance, training are nominal No airspace changes, working with current US airspace designations Communications spectrum available to support UAS Concept of operations (CONOPS) File and fly under Instrument flight rules ATC does not have direct link to the UA for flight control Fully autonomous operations not permitted Separation services will be provided to UAS Two separation thresholds. Self Separation (SST) and Collision Avoidance (CAT) Figure 5. Fig. 5. Adapted from [10, p. 3-21] 2014, Kip Johnson, All ights eserved 14

Application of STAMP-STPA Scope. Analysis and design of flight operations only Techno-human changes, challenges introduced to the NAS Air traffic management May not have control when UAS is operating autonomously (lost link) or under malevolent control (hacking) UAS operator & remote UAS operations Operator needs a way to see and avoid -> Detect and Avoid (DAA) Operator needs a way to communicate and control (C2) -> C2 Data ink Human Factors oss of visual, auditory, motion (angular & linear accelerations) Motivation for self-preservation 2014, Kip Johnson, All ights eserved 15

Application of STAMP-STPA Air Traffic Organization STPA on Technohuman level and control agents Note. System model shows importance and relationship of both C2 and DAA Safe and secure integration analysis of much more than simply C2 and DAA Airspace Control Agent To be determined Operator Small UAS ine-of Sight Control Small UAV Visual, Displays Policy, Procedures Audits Air Traffic Management Positive or Procedural Control Aircraft Control Agents Operator UAS Flight/Mission Control UAV Control System Up ink Control Displays Down ink Unmanned Aircraft Communications Flight Control System Detect & Avoid Voice, Display Data feedback Pilot Flight/Mission Control Process. Integrated Flight Operations Cooperative Coordination Visual, Tactile, Displays Manned Aircraft Flight Control System Collision Avoidance System Fig 6. Techno-Human Safety Control Structure 2014, Kip Johnson, All ights eserved 16

Overview Introduction Background Application of STAMP-STPA Conclusions 17

Conclusions We can successfully apply STAMP-STPA to the UAS-NAS integration system. STPA derived high level constraints, requirements for integration system and associated control agents UAS operator and DAA STPA Step 2 control loop models developed ffort to assist standards making committees in framing, designing, and assessing system safety Next research phase. Defining UAS human-automation ontology from STPA Develop process and method for analytical design space characterization of safety and security 2014, Kip Johnson, All ights eserved 18

Bibliography & Acknowledgments Bibliography [1] http://www.faa.gov/news/fact_sheets/news_story.cfm?newsid=14153, accessed 22 Sept 2014. [2] S. J. Zaloga, D. ockwell, and P. Finnegan, World Unmanned Aerial Vehicle Systems. Market Profile and Forecast 2013 dition., Fairfax, 2013. [3] D. D. Weatherington, Post Iraq and Afghanistan: Current and Future oles for UAS and the Fiscal Year, 2013. [4] Federal Aviation Administration, Integration of Civil Unmanned Aircraft Systems (UAS) in the National Airspace System (NAS) oadmap, 2013. [5] P. Checkland, Systems Thinking, Systems Practice. Chichester: John Wiley & Sons, Inc., 1993. [6] W. Young and N. G. eveson, An integrated approach to safety and security based on systems theory, Commun. ACM, vol. 57, no. 2, pp. 31 35, Feb. 2014. [7] https://acc.dau.mil/docs/dag_pdf/dag_ch4.pdf, accessed 2 Sept 14 [8] TCA SC-228, Detect and Avoid (DAA) White Paper, Washington, DC, 2014. [9] Federal Aviation Administration, Sense and Avoid (SAA) for Unmanned Aircraft Systems (UAS). Second Caucus Workshop eport, 2013. Acknowledgments The authors thank Dr. oland Weibel, MIT incoln aboratory Technical Staff, for research collaboration. 19