| 1. | Fuzzy neural network control with application to post - stall maneuvers
模糊神经网络在过失速机动飞行中的应用 |
| 2. | Design method of fuzzy system to control large maneuver flight of aircraft
飞机大机动飞行的一种模糊控制系统设计方法 |
| 3. | Then s - style high maneuver trajectory with high angles of attack is simulated by given control commands of angle of pitch
进行了俯仰平面s型轨迹机动飞行仿真，仿真结果说明了大攻角飞行的高机动特性。 |
| 4. | Simulation that is the developing of the flight dynamics of helicopter is the best way to study maneuver flight of helicopter
计算机仿真是研究直升机机动飞行最有力的手段，直升机仿真技术也是直升机飞行动力学发展的方向之一。 |
| 5. | Separation flow will occur when aircrafts fly at high angle , the characteristics of separation flow have an effect on aircraft performance
飞行器在做大迎角机动飞行时，流动会发生分离，而分离流的特性对飞行器的性能影响非常大。 |
| 6. | Then several typical maneuvers are picked up to simulate , and the result shows that the control system can satisfy the design specification of ads33d criteria
并且选取几个典型的机动飞行科目进行仿真，结果表明达到ads33d标准要求。 |
| 7. | Under the requirement of multi - maneuver flight mission , spacecraft sometimes has to perform autonomous navigation by using on - board sensors in a short time
未来多任务航天器往往要执行多次机动飞行,由于地面导航的局限性,需要在较短的时间内对航天器进行自主导航。 |
| 8. | In addition , a series of reasonable time histories of helicopter velocity , angular velocity and flight attitude were shown during the given dolphin maneuver flight
最后以黑鹰直升机为例计算了鱼跃越障机动飞行时驾驶员操纵输入及直升机速度、角速度和飞行姿态的变化规律。 |
| 9. | The aircraft load calculation implies determination of the loads acting on the aircraft structure for flight maneuvers , flight in turbulence , landing and ground handling conditions
飞机的载荷计算就是确定飞机在机动飞行、突风飞行、着陆和地面操作过程中作用在飞机结构上的载荷。 |
| 10. | At the end , the vibration responses are displayed in polar diagram synthetically , in which the displacement , the static offset and the deflection angle of rotor could be shown altogether
提出用极坐标表征转子振动特性的方法，可以更直观、全面地反映转子的振动幅度、机动飞行时的静态偏移以及偏摆角。 |
