| 1. | The sideslipping airplane gives rise to a side force on the vertical tail .
侧滑的飞机在垂直尾翼上引起侧力。 |
| 2. | In most flight conditions it is desired to maintain the sideslip angle equal to zero .
大多数飞行状态都要求保持侧滑角等于零。 |
| 3. | Both the sideslip angl e and the rudder angle are seen to be very much dependent on the angle of climb .
人们可以看到，侧滑角和方向舵偏角都在很大程度上依赖于爬升角。 |
| 4. | Analysis on non - sideslip equation in wheel tractor steering theory
轮式拖拉机转向理论中无侧滑方程的分析 |
| 5. | Sideslip , sharp steer and obit deviation are the often occurrence of accidents during this process
在这一过程中所发生的侧滑、激转和轨道偏离常常是行车事故的主要原因。 |
| 6. | This paper introduces two methods to get the virtual sensor signal of angle of attack and sideslip angle : nonlinear observer method and ins / gps method
本文介绍了两种方法来得到迎角和侧滑角的虚拟传感器信号：非线性观测器方法和利用ins gps系统数据估计迎角和侧滑角方法。 |
| 7. | The pressure model of flush airdata sensing system is nonlinear equations of the angle of attack , angle of sideslip , dynamic pressure and static pressure of the free stream
飞行器表面的压力分布是大气数据(迎角、侧滑角、动压、静压)的非线性函数,这个函数主要可以从空气动力学模型得到。 |
| 8. | The shm ( single hole microblowing ) as a new perturbation active control technique has been applied to the slender body with different model noses at zero sideslip and high angle of attack
摘要在亚临界流动范围内，对具有不同头部形状的尖拱形细长旋成体在无侧滑大迎角下进行单孔位微吹气扰动控制实验。 |
| 9. | The relevance functions between total pressure recover coefficient and the parameters ( mach number , angle of attack , flow coefficient , angle of sideslip ) for subsonic submerged inlet in turbojet and turbofan engine were investigated
摘要根据某埋入式进气道试验数据建立了计算埋入式亚声速进气道总压恢复系数的经验公式，表现为关于马赫数、流量系数、攻角、侧滑角的函数。 |
| 10. | The observer using the coupling of axial and lateral and having feedback of acceleration is investigated . this method can estimate the angle of attack and the sideslip angle synchronously . an optimization named extrem is applied to optimize the feedback plus matrix
研究了采用纵横向耦合且具有线加速度反馈的非线性观测器方法，该方法能够同时估计迎角和侧滑角参数，并采用extrem优化方法对其反馈参数增益参数进行了优化设计。 |
