Flight dynamic modelling and simulation of large flexible aircraft

Dussart, Ga�tan; Portapas, Vilius; Pontillo, Alessandro; Lone, Mudassir

Abstract

The drive for aircraft efficiency and minimum environmental impact is requiring the aerospace industry to generate technologically innovative and highly integrated aircraft concepts. This has changed the approach towards conceptual design and highlighted the need for modular low fidelity aircraft simulation models that not only capture conventional flight dynamics but also provide insight into aeroservoelasticity and flight loads. The key aspects that drive the need for modularity are discussed alongside integration aspects related to coupling aerodynamic models, flight dynamic equations of motion and structural dynamic models. The details of developing such a simulation framework are presented and the utility of such a tool is illustrated through two test cases. The first case focuses on aircraft response to a gust that has a spanwise varying profile. The second investigates aircraft dynamics during control surface failure scenarios. The Cranfield Accelerated Aeroplane Loads Model (CA2LM) forms the basis of the presented discussion.

Citation

Dussart, G., Portapas, V., Pontillo, A., & Lone, M. (2018). Flight dynamic modelling and simulation of large flexible aircraft. In K. Volkov (Ed.), Flight Physics - Models, Techniques and Technologies (49-72). London, UK: IntechOpen. https://doi.org/10.5772/intechopen.71050

• Publication Date: Jan 26, 2018
• Peer Reviewed: Peer Reviewed
• Pages: 49-72
• Book Title: Flight Physics - Models, Techniques and Technologies
• ISBN: 9789535138082
• DOI: https://doi.org/10.5772/intechopen.71050
• Keywords: modelling, simulation, flight dynamics, flexible aircraft, aeroelastic coupling
• Public URL: https://uwe-repository.worktribe.com/output/872050
• Publisher URL: http://dx.doi.org/10.5772/intechopen.71050