| 1. | Flight mechanics - concepts , quantities and symbols - flight points and flight envelopes
飞行点和飞行包线 |
| 2. | Flight mechanics . concepts , quantities and symbols flight points and flight envelopes
飞行力学概念量和符号飞行点和飞行包线 |
| 3. | The airplane ' s handling qualities continue to be very good throughout the flight envelope
在整个飞行包线内这架飞机的操纵品质也是相当的出色。 |
| 4. | Flight dynamics - concepts , quantities and symbols - part 7 : flight points and flight envelopes
飞行动力学.概念量及符号.第7部分:飞行点及飞行包线 |
| 5. | The design of aero - engine optimal controller suitable for all flight envelope with neural network approximator
利用神经网络设计航空发动机全包线最优控制器 |
| 6. | 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。 |
| 7. | Cnsatm systems will minimise airspace constraints and reduce traffic congestion , and this will enable aircraft to operate within their most optimum flight envelope , commensurate with achieving a marked increase in flight safety
卫星通讯、导航及监察航空交通管理系统可把空域限制减至最少，纾缓交通挤逼，从而让航机充分发挥其性能，并且大大提升飞行安全。 |
| 8. | In addition , some problems about engineering applications including the influence of regulating parameter to system control effect and the adaptability of the model following controller in flight envelope are discussed
此外，文中对控制器中的可调参数对控制效果的影响及最终滑动模态变结构模型跟踪控制器在飞行包线范围内的适应性等工程应用问题进行了讨论。 |
| 9. | A wind calculation is also provided when the uav flights along the straight course . at last , simulation in flight envelope with matlab / simulink is is offered with data and graph to prove the simulation design is successful
最后,通过matlab / simulink实现了无人机全过程飞行的非线性仿真验证,分析了无人机在全航程飞行过程中的飞行数据/曲线,验证了本文研究内容的正确性。 |
| 10. | A mathematical model reflecting the tilt rotor unsteady and nonlinear aerodynamic characteristics in the longitudinal channel is presented in the paper . in the full flight envelope , the rotor thrust continues tilting and the aerodynamic forces of each component change as a function of airspeed and nacelle angle
在整个飞行包线内,旋翼的推力矢量方向不断变化,飞机各部件的气动力随发动机短舱倾角和空速的变化而变化,因而飞机的飞行动力学有很强的非定常、非线性特性。 |
