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公开(公告)号:US4834318A
公开(公告)日:1989-05-30
申请号:US130946
申请日:1987-12-10
申请人: Paul Taylor , Jane M. Thorpe , Alistair C. Graham
发明人: Paul Taylor , Jane M. Thorpe , Alistair C. Graham
CPC分类号: B64C27/72 , G05D1/0858 , Y02T50/34
摘要: In a helicopter, signals representative of the rotor disc attitude of a main sustaining rotor (11) are fed into a flight control system (24) to modify an actuator demand signal (31) controlling a rotor blade actuation system (32) of the main sustaining rotor.