| 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. | Nonlinear bifurcation analysis on post - stall transients of axial - flow compressor
轴流压缩系统过失速行为的非线性分叉分析 |
| 3. | Simulation results are presented over a range of flight conditions to confirm the effectiveness of the design
以此为基础我们还对一过失速机动作了仿真分析。 |
| 4. | When the missile attack process is simulated , the application of post stall maneuvers provides significant advantages
在模拟导弹攻击目标时，采用过失速机动控制模式具有明显的优势。 |
| 5. | Using this method , the flight control law which suits to the vectored aircraft flight in post - stall domain is designed in this paper
运用这种方法对推力矢量飞机进行了适用于过失速机动的非线性飞行控制系统设计。 |
| 6. | The post - stall behavior and recoverability of compression systems are studied theoretically and experimentally in this paper respectively
本文分别对轴流压缩系统过失速性能和失速可恢复性两方面的问题进行了理论和实验研究。 |
| 7. | The thrust vectoring control technology and post - stall maneuverability enhance the aircraft ' s combat effectiveness greatly , and cause the worldwide interest
推力矢量控制技术和过失速机动使战斗机的空战效能大大增加，引起了世界各国的关注。 |
| 8. | The results show that there are no un - receptible responses when the post stall maneuver modes are applied , and agility is raised significantly
试验结果表明，使用的4种过失速机动控制模式没有不可接受的操纵响应，飞机采用推力矢量控制后敏捷性明显提高。 |
| 9. | The results show that the control law can control vectored aircraft to accomplish post - stall maneuvers very well and it is very robust to model uncertainty . 4
仿真结果表明，该控制律能控制推力矢量飞机顺利完成过失速机动，对系统模型的不确定性具有较强的鲁棒性。 |
| 10. | The application of thrust vectoring control technology makes the aircraft possess the ability to fly in post - stall domain , therefore the flight envelope is extended
推力矢量控制技术在战斗机上的应用，使战斗机有能力进入过失速飞行领域，使飞机的飞行包线得以扩展。 |
