07 - Systems, Subsystems and Equipment
SIMPLIFIED MODELS OF PILOT BIOMECHANICS FOR ROTORCRAFT VERTICAL BOUNCE ANALYSIS
T. Aresi¹, A. Zanoni¹, G. Cassoni¹, P. Masarati¹; ¹Politecnico di Milano, Italy
The paper addresses the rotorcraft-pilot coupling problem, where induced vibrations affect the control system through pilot-operated control sticks. It introduces an analytical multibody description of the vertical bounce issue to enhance understanding, facilitate comparison with prior studies, and establish control synthesis models. Parameters are identified through tests for model comparison.