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@inproceedings{Roberto2008Shipboardb,

title = {Individual Blade Root Control of Helicopter Blade Sailing for Hingeless Shipboard Rotors},

author = {Roberto Luiz Cunha Barroso Ramos and Donizeti Andrade and Luiz Carlos Sandoval G\'{o}es},

url = {https://www.sige.ita.br/edicoes-anteriores/2008/st/11_3.pdf},

year  = {2008},

date = {2008-01-01},

booktitle = {Simp\'{o}sio de Aplica\c{c}\~{o}es Operacionais em \'{A}reas de Defesa 2008 (SIGE2008)},

abstract = {This paper investigates an individual-blade-root- control approach to the reduction of helicopter blade sailing in hingeless rotors, considering steady flow conditions during theoretical engagement shipboard operations and using aeroservoelasticity principles. The aeroelastic control law individual-blade-root synthesis yields a flap-state-feedback lift/angle-of-attack compensation whose controller for the parameters are associated with the damping/stiffness enhancement of the flapping motion. The simulation results show that the proposed aeroservoelastic controller can obtain blade-sailing reduction of nearly 30% in upward and downward deflections at severe wind-over-deck conditions by using low blade pitch input limits of the actuators. This blade-sailing reduction can prevent tunnel/tail-boom strikes from occurring. Keywords Shipboard helicopter, blade sailing, individual blade root control, hingeless rotor, aeroservoelasticity.},

keywords = {aeroservoelasticity, blade sailing, hingeless rotor, individual blade root control, Shipboard helicopter},

pubstate = {published},

tppubtype = {inproceedings}

}