发明授权
US4834318A Helicopter flight control systems 失效
直升机飞行控制系统

Helicopter flight control systems
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.
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