Before entering into operation, new aircraft must obtain a type certificate from the governing aviation regulatory authority. This certificate testifies that the type of aircraft meets the safety requirements. After the definition of the certification basis, the aircraft manufacturer and the authority must agree on the certification program structure and on how to demonstrate regulation compliance. This compliance demonstration is the most expensive and time-consuming aspect of the certification process, involving high safety risk concerning control system and engine failures. Advanced analysis methods as flight simulation potentially offer an immediate benefit in the certification process for cost/time saving and risk reduction.
RoCS aims to explore the possibilities, limitations, and develop guidelines for best practices for the application of flight simulation to demonstrate compliance to the airworthiness regulations related to helicopters and tiltrotors. While flight simulation cannot fully replace all flight-testing activities, it allows reducing the number of flight tests with respect to current certification standards, within the OFE. Further tests outside the OFE that may lead to catastrophic failure could be conducted by flight simulation.
A three-way approach defines RoCS objectives:
• Developing guidelines for certification of rotorcraft using simulation by consolidating past experiences and dedicated research into a set of guidelines, supported by both industry and the certification authority, defining model and cueing system fidelity metrics. RoCS will develop a set of standard tools to evaluate these metrics in a fast, efficient, and reliable way.
• Developing a low-cost, effective, flight simulation environment for certification compliance demonstration for helicopters and tiltrotors, replacing the concept of flight simulation just for training. This will lead to the development of a new class of simulators that will be competitive to flight tests in terms of acquisition and maintenance costs, affordable also by small rotorcraft companies, and a driver in the development process for certifying aircraft.
• Verifying if certification by simulation could reduce the scope of testing required for the introduction of the next generation of tiltrotors. This final ambitious goal, reached through the issue of final guidelines for CSRFA verified on tiltrotors, will represent a formidable tool to compensate for the lack of experience of both the manufacturers and the certification authorities in using simulation to support certification. It will limit significantly the amount of potentially hazardous flight-testing currently performed in the certification process.