A New Heuristic Approach to Rotorcraft System Identification

A New Heuristic Approach to Rotorcraft System Identification

High-fidelity rotorcraft flight simulation relies on the availability of a quality flight model that further demands a good level of understanding of the complexities arising from aerodynamic couplings and interference effects. This paper explores rotorcraft flight dynamics in the low-speed regime w...

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Bibliographic Details
Main Authors: Agarwal, D. (Author), Cameron, N. (Author), Lu, L. (Author), Padfield, G.D (Author), White, M.D (Author)
Format: Article
Language:English
Published: American Helicopter Society 2023
Subjects:
Aerodynamic couplings
Aerodynamic interference
Aircraft
Coupling effect
Flight dynamics
Flight models
Flight simulators
Heuristic methods
Heuristics approaches
High-fidelity
Interference effects
Low speed
Rotorcraft flight simulation
System-identification
Wakes
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