| 摘要 |
An angle-of-attack/attitude fluidic flight control system with gain changer means for compensating for output signal sensitivity to flight velocity variations including angle-of-attack sensor means for generating an output signal sensitive to the flight velocity and the angle-of-attack of a vehicle in flight, gyro means fluidically connected to the angle-of-attack sensor means for receiving a fluid pressure supply therefrom, the gyro means providing an output signal sensitive to the flight velocity and the attitude of the vehicle in flight, summer-integrator means having an input fluidically connected to the angle-of-attack sensor means and the gyro means for receiving the output signals therefrom, the output signals from the angle-of-attack sensor means and the gyro means being compared at the input of the summer-integrator means, and the summer-integrator means having an output connectable to actuator means for providing thereto correction signals for maintaining through operation of the actuator means the desired angle-of-attack and attitude of the vehicle in flight.
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