The algorithm has been embedded in the attitude control system of a small unmanned helicopter.
该算法已应用于小型无人直升机的姿态控制中。
The control algorithm of attitude follow-up stabilization and tracking antenna platform adopts position feed-forward control, speed control and position feedback control.
姿态随动稳定跟踪天线平台的控制算法，采用位置前馈、速度和位置反馈控制。
With this measured data, information fusion algorithm is able to design a high precision Attitude and Heading Reference system. Therefore it can accord with the control system demand.
依据这些原始数据设计适当的信息融合算法可以构建高精度的姿态航向参考系统，从而满足控制系统的要求。
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