片语

all-attitude angle全姿态角

roll attitude angle滚转姿态角

attitude e angle姿态角

gun attitude angle火炮姿态角

attitude large angle slew姿态大角度机动

attitude angle transducer姿态角传感器

aircraft attitude angle飞机姿态角

attitude angle sensor姿态角传感器

英汉例句

• the attitude angle of high-speed mobile object in the shield tube is tested by use of optical lever in this paper.

  采用光学杠桿的方法对遮蔽管内的高速运动物体进行姿态角测试。

• subsequently, the control loop of attitude angle is designed with dynamic inversion scheme.

  随后本文基于动态逆思想设计了武装直升机姿态角控制回路。

• the method is simple, requires little computation. the relative position and attitude angle of the trace spacecraft can be given through measuring.

  这种方法简单所需的运算量也较少，通过测量能给出追蹤飞行器相对于目标飞行器的位置和姿态角。

• in this paper a method for measuring the relative position and attitude angle of the spacecraft during rendezvous and docking.

  本文叙述了一种测量空间飞行器交会对接过程中位置和姿态角的方法。

• the effect that the position and light intensity of the interferential celestial bodies「 spot on the output attitude angle of the digital sun sensor(dss) was analyzed.

  分析了天体干扰光斑的位置和光强对卫星数字式太阳敏感器姿态角输出的影响。

• taking into account properties of the geomagnetic field, a new pd magnetic control law using the feedback information of attitude angle and attitude rate is developed.

  根据极地轨道地磁场变化的特性，利用卫星的姿态角和姿态角速率作为反馈信号， 提出了一种采用磁力矩器的比例微分（pd）控制规律设计方法。

• there are many methods to measurement the flying attitude, such as solar attitude angle sensor, high-speed photography and geomagnetic field sensor.

  飞行体的姿态测试方法有许多种，如太阳方位角传感器遥测、高速摄影法、地磁传感器等。

• the measurement process of the attitude angle based on single trailing earth horizon sensor is investigated, and an analytical formula of attitude compensating error is obtained.

  基于单轨迹地平仪研究了地平仪测量姿态角的过程，得到了解析形式的姿态角误差补偿公式。

• a filter design for rendezvous and docking with non-cooperative target was also given which can provide estimation information of relative position, velocity, attitude angle and angular rate.

  设计了针对空间非合作目标对接段的滤波器，能够提供对接段相对位置、速度、姿态角及角速率估计信息。

• after analysed recognition criteria, an horizon detection algorithm and transform formula for attitude angle are attained.

  文中给出了地平线判别準则及相应的算法和姿态角变换公式。

• the method to aquire the angle of attack and sideslip approximately in engineering by the deviation between apparent acceleration and attitude angle was analyzed, and the control model was given.

  研究了工程上用实时视加速度与姿态角偏差近似获得实时攻角和侧滑角的方法，并给出了控制模型。

• besides, the attitude update is used based on the open-loop kalman filtering structure, further decreasing the effects of the attitude angle errors on the positioning accuracy.

  此外，在开环卡尔曼滤波器结构基础上引入了姿态阵修正，进一步减小捷联系统姿态角误差对导航定位精度的影响。

• finally, the dissertation designed the fuzzy pd controller of trajectory tracking, which is combined with attitude angle controller, so that the whole flight controller is completed.

  本文最后设计了直升机模糊pd轨迹跟蹤控制器，与姿态角控制器相结合，完成对整个飞行控制系统的设计。

• compared with the whole attitude angle matching recognition methods, the proposed method need small memory space and small calculation time.

  与一维距离像全姿态角匹配识别方法比较，具有计算量、存贮量较小的特点。

• attitude angle is the angle between the chord of the wing and the horizon.

  介于「翼弦」跟水平面间的角度。

• it could unify people」s knowledge of the attitude angle and be of assistance in the development of rolling bearing dynamics.

  这种算法不仅能使人们对姿态角这一原本较难处理的动力学参数有一个清晰的认识，无疑也有助于滚动轴承动力学的发展。