departure angle

In this paper the definitions of approach angle, departure engle and ramp angle of a motor vehicle defined by Japan Automobile Standardization Organization ( JASO) are presented.

介绍了日本汽车标准化协会（JASO）对汽车接近角、离去角和纵向通过角的定义。

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a computing method of departure angle of multiple poles and program design for root loci

多重极点出射角计算方法研究及求根轨迹程序设计

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the result shows that the effects of variation of departure angle, initial error, variation of propellant temperature and crosswind on distance were less under the conditions of equal spin-number.

结果表明，射角变化、初速误差、发射时药温变化、弹道上横风对同样转数的飞行距离影响较小；

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ion departure angle changes periodicity, and increases with the magnetic field in parallel board direction.

打到基板上的离子的偏移角具有周期性的变化，并且随着磁场平行基板方向分童的增大而增大。

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in this paper, the computing method and formulas of departure angle of root loci for the closed loop control system with multiple poles are advanced and the computer program for seeking root loci is compiled using the newton-raphson iterative method which is put forward.

本文提出了当闭环系统特征方程具有多重极点时，根轨迹在极点处的出射角的计算方法和公式，并利用Newton-Raphson迭代法编制了求取控制系统根轨迹的计算机程序。

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Departure angle: back-end automotive primer highlights the tangent to the rear of the angle with the ground.

离去角：汽车后端突出点向后轮引的切线与地面的夹角。

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furthermore, the magnetic field cannot change the total energy density distribution of ions, but the lorentz force does influence its movement state, and at the same time affects the ion energy distribution in every directions, as well as the incidence departure angle of ions.

此外，虽然磁场不能改变离子总的能量密度分布，却能改变离子的运动状态，并同时影响着基板上离子在各个方向上的能量分布和入射偏移角度。

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thus the maximum horizontal range is attained when the departure angle is 45 °.

因此，当发射角为45°时，有最大水平射程。

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Only a large triangle could possibly reveal any significant departure from an angle sum of 180� �.

只有在大的三角形中0趴赡芟允境?80°与三角和有任何差距.

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through simulation, the estimation angle of arrival, departure angle and delay are achieved.

接着对SAGE算法做了归纳，在多径情况下，通过仿真实现离开角度、到达角和延时的估计。

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research on testing system of artillery axis consistency and departure angle

火炮轴线一致性与偏离角测试系统研究

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Analysis of Departure/ Spin Characteristics of F-16 at High Angle of Attack

F-16飞机大迎角飞行偏离/尾旋特性分析

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