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Integrated Helicopter Survivability Cranfield University Nicholas G. Law Integrated Helicopter Survivability Aeromechanical Systems Group Cranfield Defence and Security PhD DSTL/PUB36228 Cranfield University Cranfield Defence and Security Aeromechanical Systems Group PhD 2011 Nicholas G. Law Integrated Helicopter Survivability Supervisor: Prof. Kevin Knowles May 2011 © Crown copyright 2011. Published with the permission of the Defence Science and Technology Laboratory on behalf of the Controller of HMSO. DISCLAIMER Any views expressed are those of the author and do not necessarily represent those of Dstl, MOD or any other UK government department. ABSTRACT A high level of survivability is important to protect military personnel and equipment and is central to UK defence policy. Integrated Survivability is the systems engineering methodology to achieve optimum survivability at an affordable cost, enabling a mission to be completed successfully in the face of a hostile environment. “Integrated Helicopter Survivability” is an emerging discipline that is applying this systems engineering approach within the helicopter domain. Philosophically the overall survivability objective is ‘zero attrition’, even though this is unobtainable in practice. The research question was: “How can helicopter survivability be assessed in an integrated way so that the best possible level of survivability can be achieved within the constraints and how will the associated methods support the acquisition process?” The research found that principles from safety management could be applied to the survivability problem, in particular reducing survivability risk to as low as reasonably practicable (ALARP). A survivability assessment process was developed to support this approach and was linked into the military helicopter life cycle. This process positioned the survivability assessment methods and associated input data derivation activities. The system influence diagram method was effective at defining the problem and capturing the wider survivability interactions, including those with the defence lines of development (DLOD). Influence diagrams and Quality Function Deployment (QFD) methods were effective visual tools to elicit stakeholder requirements and improve communication across organisational and domain boundaries. The semi-quantitative nature of the QFD method leads to numbers that are not real. These results are suitable for helping to prioritise requirements early in the helicopter life cycle, but they cannot provide the quantifiable estimate of risk needed to demonstrate ALARP. i Abstract The probabilistic approach implemented within the Integrated Survivability Assessment Model (ISAM) was developed to provide a quantitative estimate of ‘risk’ to support the approach of reducing survivability risks to ALARP. Limitations in available input data for the rate of encountering threats leads to a probability of survival that is not a real number that can be used to assess actual loss rates. However, the method does support an assessment across platform options, provided that the ‘test environment’ remains consistent throughout the assessment. The survivability assessment process and ISAM have been applied to an acquisition programme, where they have been tested to support the survivability decision making and design process. The survivability ‘test environment’ is an essential element of the survivability assessment process and is required by integrated survivability tools such as ISAM. This test environment, comprising of threatening situations that span the complete spectrum of helicopter operations requires further development. The ‘test environment’ would be used throughout the helicopter life cycle from selection of design concepts through to test and evaluation of delivered solutions. It would be updated as part of the through life capability management (TLCM) process. A framework of survivability analysis tools requires development that can provide probabilistic input data into ISAM and allow derivation of confidence limits. This systems level framework would be capable of informing more detailed survivability design work later in the life cycle and could be enabled through a MATLAB® based approach. Survivability is an emerging system property that influences the whole system capability. There is a need for holistic capability level analysis tools that quantify survivability along with other influencing capabilities such as: mobility (payload / range), lethality, situational awareness, sustainability and other mission capabilities. It is recommended that an investigation of capability level analysis methods across defence should be undertaken to ensure a coherent and compliant approach to systems engineering that adopts best practice from across the domains. Systems dynamics techniques should be considered for further use by Dstl and the wider MOD, particularly within the survivability and operational analysis domains. This would improve understanding of the problem space, promote a more holistic approach and enable a better balance of capability, within which survivability is one essential element. There would be value in considering accidental losses within a more comprehensive ‘survivability’ analysis. This approach would enable a better balance to be struck between safety and survivability risk mitigations and would lead to an improved, more integrated overall design. ii ACKNOWLEDGEMENTS I would like to thank the following people for their support and inspiration during this work: Prof Kevin Knowles Cranfield University, Project Supervisor Mr Sam Wells OBE Dstl, Project Sponsor Dr Jim Wickes Dstl, Chief Technologist Survivability Mrs Marilyn Gilmore Dstl, Technical Advisor Signature Control Mr Tim Moores Research Director Air and Littoral Manoeuvre Mr Jan Darts SIT DTIC Air Integrated Technology Team Leader Mrs Debbie Edgar Dstl, Team Leader Rotorcraft Survivability Mr John Bowker Dstl, Team Leader Air Platform Protection Prof Dave Titterton Dstl, Technical Leader Laser Systems Mr Peter Haynes Dstl, DAS Rotorcraft Support Leader I would also like to thank Dstl Air and Weapons Systems Department for providing and funding this research opportunity. To my colleagues at Dstl who have helped to develop and apply the research in this area. Finally to my wife Rachel and son Thomas for being so understanding. iii CONTRIBUTIONS OF THE CANDIDATE This research draws upon existing and developing knowledge and understanding within the survivability domain. The candidate works within a team and consequently methodologies, models and techniques are often developed as part of a team effort. The candidate’s personal contributions to new knowledge in this discipline are as follows (‘novel’ contributions have been marked with an asterisk): Research and organisation of relevant material into one place and combining this with new ideas to further understanding within the helicopter survivability field: Survivability ‘level’ definitions with respect to helicopters (Section 1.4.3). Literature search on helicopter threats and survivability attributes (Chapter 2). Literature search on analytical methods, including Quality Function Deployment (QFD) and the Analytical Hierarchy Process (AHP) (Section 3.11). Application of a systems engineering approach to helicopter survivability and development of a survivability assessment process* (Chapter 4). The idea to apply the concept of reducing risk to ‘as low as reasonably practicable’ (ALARP) to the survivability problem* (Chapter 4). Application of the QFD method to the problem and the development of a new ‘hybrid’ risk and QFD based approach (Section 4.6.2). The idea to use a probabilistic fault tree method set around the pillars of survivability to evaluate a survivability metric and the subsequent development of the Integrated Survivability Assessment Model (ISAM)* (Section 4.8). Lessons learnt in terms of the utility of the different methods resulting from their application to the helicopter acquisition process. (Chapters 4 and 5). v TABLE OF CONTENTS ABSTRACT ............................................................................................................................................................ i ACKNOWLEDGEMENTS ................................................................................................................................. iii CONTRIBUTIONS OF THE CANDIDATE ...................................................................................................... v TABLE OF CONTENTS .................................................................................................................................... vii TABLE OF FIGURES ......................................................................................................................................... xi TABLE OF TABLES ......................................................................................................................................... xiii NOMENCLATURE ............................................................................................................................................ xv PROBABILITY RELATED TERMS .......................................................................................................................... xv POWER REQUIRED FOR GENERAL FORWARD FLIGHT TERMS ............................................................................... xv ABBREVIATIONS .............................................................................................................................................
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