| 摘要 |
The handling capability of helicopters at high speed is enhanced by applying a force to the cyclic stick which is related to the resultant load factor induced on the helicopter by movement of the cyclic stick by the pilot. A feed augmentation system responds to craft pitch rate, cyclic stick deflection and cyclic stick deflection rate signals as a function of airspeed to provide a control force feel on the cyclic stick that does not vary with speed. Both pitch and roll axis controls can be provided.
|
