This open access book presents the steps necessary for the application of rotorcraft flight modelling and simulation and analysis in support of certification for compliance with EASA CS-27 and CS-29, SUBPART BFLIGHT and other flight-related rules (e.g. CS-27/9, Appendix B, Airworthiness Criteria for Helicopter Instrument Flight). The material is presented in the form of a structured 'Rotorcraft Certification by Simulation' process, starting from the relevant paragraphs in the Certification Specifications, through a comprehensive description of the assembly of flight simulation requirements, informed by judgements on Influence, Predictability and Credibility, and on into the detailed building of the three major elements of the process; the Flight Simulation Model, the Flight Simulator, and the associated Flight Test Measurement System. The latter feeds both the flight model and simulator development with real-world test data to support validation and fidelity assessment. The book is intended to provide support to early adopters of simulation and analysis in the certification process, including those who have considerable experience and expertise in the use of Modelling and Simulation in support of design and development. It is acknowledged that there exists much good practice in the rotorcraft industry in this regard. However, what is presented herein is considered a significant step forward in the development of this practice, particularly in terms of the importance of a structured, requirements-based, process using adaptable-fidelity, descriptive and predictive simulation tools, and associated pre-certification flight testing, to reach the goal of a credible flight simulation.

This book is open access, which means that you have free and unlimited access Builds a framework for the use of modelling and simulation in support of rotorcraft certification Showcases the benefits of RCbS capability in terms of certification time & cost, energy consumption, safety, performance Written by experts in the field from both academia and aerospace research centers

Autorentext

Stefan van’t Hoff is Principal R&D Engineer and Leads the Vertical Flight team at NLR, the Netherlands. Philipp Hofmeister is a R&D Engineer at the Institute of Flight Systems – Rotorcraft Department at DLR, Germany. Linghai Lu is Senior Lecturer in Flight Dynamics and Simulation at Cranfield University, UK. Gareth D. Padfield is Emeritus Professor of Aerospace Engineering at The University of Liverpool, UK. He is the Book lead editor. Giuseppe Quaranta is Professor of Aeroservoelasticity, and Deputy Head at the Department of Aerospace Science and Technology of Politecnico di Milano, Italy. He was the RoCS project lead. Mark White is Professor of Aerospace Engineering and Head of the Department of Mechanical and Aerospace Engineering at The University of Liverpool.

Inhalt

1. Introduction.- 2. Structure of the RCbS Process.- 3. Developing the RCbS Project Management Plan (Phase 0).- 4. Requirements Capture and Build (Phase 1).- 5. Rotorcraft Flight Modelling and Simulation.- 6. Flight Simulation Model Development (Phase 2a).- 7. Flight Simulator Development (Phase 2b).- 8. Flight Test Measurements for FSM/FS Development (Phase 2c).- 9. Credibility Assessment and Certification Activity (Phase 3).- 10. Resourcing the RCbS Process.- 11. Guidance for Selected ACRs within the Certification Specifications.- 12. Case Study 1: CS-27/29 Low Speed Controllability and Manoeuvrability.- 13. Case Study 2: CS 29/27 Category A Confined Area Rejected Take-off.- 14. Case Study 3.- 15. Finale and Potential Routes to the Adoption of RCbS.