侧滑角的英文

• angle of side slip
• angle of sideslip
• angle of slide
• attitude angle
• side sliangle
• slip angle
• yaw angle

• "侧滑"英文翻译    sideslip; sideslipping gliss ...
• "角"英文翻译    role; part; character
• "大侧滑角的" 英文翻译 :    highly yawed; highly-yawed
• "平衡侧滑角" 英文翻译 :    equilibrium side-slip angle
• "侧滑角指示器" 英文翻译 :    angle-of-sideslipping indicator
• "带侧滑角的管" 英文翻译 :    yawed tube
• "侧滑角改变装置" 英文翻译 :    yawing mechanism
• "空气动力对侧滑角的导数" 英文翻译 :    aerodynamic derivative with respect to sideslip
• "偏航力矩寻侧滑角曲线" 英文翻译 :    curve of yawing moment versus sideslip angle
• "滑角" 英文翻译 :    sa sliangle; slip angle
• "侧滑" 英文翻译 :    1.[航空] (飞机对称面和相对气流方向不一致的飞行) sideslip; sideslipping2.(芭蕾舞横滑步) glissade◇侧滑机翼 sideslipping wing; 侧滑角 angle of the sideslip; 侧滑特性 side-slip characteristics; 侧滑仪 slip indicator; 侧滑指示器 clinoscope
• "抗滑角" 英文翻译 :    angle of resistance; resistance angle
• "偏滑角" 英文翻译 :    slip angle
• "起滑角" 英文翻译 :    angle of slide
• "前滑角" 英文翻译 :    advance angle; no-slip angle
• "视滑角" 英文翻译 :    apparent planing angle
• "下滑角" 英文翻译 :    glide angle; glide path angle; gliding angle
• "侧滑，横滑" 英文翻译 :    side slide
• "侧滑步" 英文翻译 :    side step; slip step
• "侧滑轨" 英文翻译 :    wood side-guide
• "侧滑块" 英文翻译 :    side slide
• "侧滑力" 英文翻译 :    skid force
• "侧滑轮" 英文翻译 :    side roller
• "侧滑片" 英文翻译 :    yaw vane
• "侧滑移" 英文翻译 :    side slip

• 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。
• 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。
• 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。
• 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。
• 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。
• An improved iteration is presented based on the simplification by general inverse of matrix . the improved iteration contains only one iterate variable . thus , it can be analyzed easily of its convergence and it can work faster than the original iteration
  总压、动压修正比,与迎角和侧滑角一起,包括了计算动压和静压的足够信息,并且在求解精度上是原始方程组的最小二乘解。
• 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。
• The angle of attack and the sideslip angle are the two important measured quantities for the aircraft navigation / control aerodynamics analysis and structure analysis . for the different kinds of disturbance influence , now the sensors ca n ' t measure it accurately , in the high angle of attack , the error will add with the angle of attack increase
  迎角和侧滑角是飞机飞行导航控制、航电等方面重要的两个测量量，由于受到各种干扰因素的影响，现代传感器很难对其精确测量，在超大迎角飞行过程中，其测量误差随迎角增加而增加。
• 3 . the project using ins / gps system data to estimate the angle of attack and sideslip is brought forward first . this project using the ins / gps system data , such as acceleration and velocity signal , and others signals of the aircraft , such as gyros and the mathematic models , to estimate virtual signal
  首次采用ins gps系统数据来估计迎角和侧滑角传感器参数原理和方法，利用ins gps系统测量的地速和总加速度信号结合飞机其他传感器和数学模型估计得到了迎角和侧滑角传感器的虚拟信号，该种方法具有很好的实时性。
• The formula for mach number has been optimized with least - squres solution , thus the precision of a polynomial of power of 5 is better than that of 9 . 2 . after the solving of angle of attack and angle of sideslip , the theory of general inverse of matrix is used to simplify the nonlinear equations and to calculate the total pressure and the modified dynamic pressure ratio . these two parameters together with the angle of attack and angle of sideslip contain enough information to work out the dynamic pressure and static pressure
  其中包括: 1 .应用最小二乘法,对马赫数的泰勒求解公式进行优化,优化后的求解公式采用5次多项式即可在精度上优于原有的9次多项式,可以提高运算速度; 2 .提出应用广义逆矩阵简化非线性方程组:在已经求解出迎角与侧滑角的前提下,直接从原始的压力向量中提取出总压,并且提出了动压修正比的概念。

• 侧滑角的法语：angle de dérapage
• 侧滑角的日语：スリップアングル へんりゅうかく スリップかく よこすべりかく サイドスリップアングル よこながれかく スリップ角
• 侧滑角的俄语：угол вращения вокруг вертикальной оси
• 侧滑角的阿拉伯语：زاوية الانعراج;