| 摘要 |
<p>This system provides means for computing the forces and moments on and developed by the rotary wing of rotary-wing aircraft for realtime simulation purposes. The system includes a plurality of control signal generators for generating information relating to various components of rotary-wing aircraft and means to compute from these resultant signals quantities representative of the final resultant forces on the aircraft, its rotary wing, and other components. In particular, this specification describes equipment for computing the forces and moments developed by and on the rotary wing by utilizing aircraft design data and data produced in actual flight tests.</p> |
