在相同航迹角航行情况下，水平方向速度随净浮力的增大而增大。
And the more excess mass the faster speed is at the same track angle.
适当地结合规划-跟踪算法和航迹角控制器可给再入制导带来极大的灵活性和适应性。
Proper combination of planning-tracking algorithm and FPA controller can bring great flexibility and adaptability to reentry guidance.
航迹角修正法的采用，进一步修正了规划出的飞行轨迹，从而获得了理想的飞行参考轨迹。
After adopting the correcting method of flight path Angle, flight path planned is further modified and ideal reference flight path is obtained.
用航迹角来代替性能计算中常用的爬升率概念，对飞机爬升各项参数的变化及其影响因素进行了研究。
In this article, trajectory angle is taking the place of the rate of climb in order to study the influence of other trajectory parameter applied on it.
以涡轮和火箭冲压组合动力的工作模式以及飞行器飞行航迹角、迎角等为调参量，构造空天飞行器爬升轨迹优化流程。
The flow chart of optimizing ASP climb track is designed by adjusting some parameters of Euler angle, attack angle, turbine and rocket-ramjet combined cycle work models, etc.
着重分析了舰载飞机在下滑过程中，雄鸡尾流对过载以及雄鸡尾流水平加速度、铅垂加速度对航迹角、下沉率和附加需用推力的影响。
The effects of the cocktail on overload, the level and vertical acceleration on flight path Angle, sinking velocity and extra required propulsion were analyzed during the glide of the aircraft.
提出了利用速度向量及位置信息求取照射角的方法，并与航迹外延法求照射角作比较，提出了基于照射角的雷达调度策略。
The method of obtaining it by using the velocity vector and location information is put forward, which is compared with the method of track extrapolation.
当船舶或船队的尺度确定后(主要是长和宽)，航道宽度即取决于航迹带宽度，而航迹带宽度又取决于航行漂角的大小。
As the ship or fleet size is defined, the channel width is dependent on the track zone width, and track zone width is dependent on the drift Angle of navigation.
提出采用一种结合三角网格退化、变域动态规划以及航迹优化的方法来解决突发威胁下的航迹规划问题。
This method combined the ameliorated grid degenerate and dynamic programming, it can solve the problem of time delay in path planning with sudden appearing threats.
针对原系统图形换屏显示时船舶航迹有时位于屏幕一角及航迹偏差带有时宽窄不一致的问题，重新设计了换屏技术及采用了新的偏差带的画法，根据船舶运动计划航线决定船舶进入屏幕的点，保证了船舶位于屏幕中部。
A new method of changing screen is adopted and the point where ship drives into the screen is determined in accordance with the ship's course to make the ship located at the middle of the screen.
对一个高超声速飞行器设计了滑动模态观测器来估计攻角和航迹倾角。
A sliding mode observer is designed to estimate the Angle of attack and flight path Angle for a hypersonic vehicle.
修正基于航迹的刚体目标姿态角计算方法，避免模型切换时的姿态角振荡现象，便于相关应用的实现。
It revises the way to obtain the pose Angle of the rigid body target based on track, avoids the pose surge when the model changes, and it is a good reference for relevant applications.
修正基于航迹的刚体目标姿态角计算方法，避免模型切换时的姿态角振荡现象，便于相关应用的实现。
It revises the way to obtain the pose Angle of the rigid body target based on track, avoids the pose surge when the model changes, and it is a good reference for relevant applications.
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