论文信息 - Modeling and linear function parametric identification for a helicopter main rotor

Modeling and linear function parametric identification for a helicopter main rotor

A model of a helicopter test rotor obtained according to the Euler-Lagrange approach is presented. A simplified linear representation for this model, suitable for control system design, is also proposed. The dynamics of the helicopter test rotor are identified in terms of its linearized model by applying the Strej method.

Rafael Castro-Linares | Eduardo Liceaga-Castro | José M. Molinar-Monterrubio

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