• A method to limit the amplification in a certain range is proposed for restricting the big estimated error of pitch attitude angle.

    本文还提出了限定增益系数的方法,以抑制俯仰角过大的估计误差。

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  • 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。

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  • Attitude measurement was the measurement of attitude Angle.

    姿态测量也就是对姿态角的测量。

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

    采用光学杠杆的方法对遮蔽管内的高速运动物体进行姿态角测试。

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  • The attitude Angle (or angular rate) data of INS were often ignored during study and application of automatic alignment technique.

    在以往的自对准技术研究与应用中,惯导系统的姿态角(或角速率)信息往往是被忽略不用的。

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  • The composition and principle of the platform were introduced, and the error equations of attitude Angle, velocity and position were given.

    介绍了平台的组成及工作原理,并且推导出平台角误差方程、速度误差方程和位置误差方程。

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  • 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,通过测量能给出追踪飞行器相对于目标飞行器的位置和姿态角。

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  • 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。

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  • 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。

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  • Furthermore, the computer simulation technique is applied to study initially the distortion law of CCD satellite images caused by errors of ephemeris parameters and initial attitude Angle.

    利用计算机仿真技术初步研究了星历参数和初始姿态角误差引起的CCD卫星影像畸变的规律。

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  • 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。

    youdao

  • 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。

    youdao

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