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大多数框架式平台,鉴定其初始对准的标准方法,不是采用光学方法来监控稳定的平台,就是移动惯性平台(如:火箭撬测试)来测量其纵横向误差。令人遗憾的是,先进惯性参考球是一个液浮、球型的惯性平台,没有光学信息接至平台。因此,唯一的姿态信息是一个比较粗糙的读出系统,以此提供信息至导弹自动驾驶仪。本文提出了一种技术,用这种技术来校准姿态系统和鉴定先进惯性参考球平台的方位瞄准。值得注意的是,所提出的技术不仅使先进惯性参考球平台的方位瞄准与天文参考系精确地连系起来,而且既没有与方位瞄准机构,也没有与控制的卡尔曼滤波器及其与平台的相互作用发生矛盾。
Most frame-based platforms, the standard method of identifying their initial alignment, do not use optical methods to monitor a stable platform or to move the inertial platform (eg, a rocket pry test) to measure its longitudinal and lateral errors. Unfortunately, the advanced inertial reference ball is a floating, spherical, inertial platform with no optical information attached to the platform. Therefore, the only attitude information is a relatively coarse readout system to provide information to the missile autopilot. This paper presents a technique that uses this technique to calibrate the attitude system and identify the azimuth targeting of advanced inertial reference ball platforms. It is noteworthy that the proposed technique not only enables the azimuth aiming of the advanced inertial reference ball platform to be precisely linked with the astronomical reference frame but also does not relate precisely to the azimuth targeting mechanism nor to the controlled Kalman filter and its platform Conflicts occur in the interaction.