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。
DSP controller is chose as the system CPU and the attitude control demo experiment is achieved by generalized the incomplete integral PID control algorithm.
采用不完全积分PID控制算法初步实现了姿态控制的演示实验。
To solve the attitude maneuver of a flexible satellite, this article presents a variable structure tracking control algorithm based on output feedback.
为解决柔性航天器姿态机动的控制问题，给出了基于输出反馈的变结构跟踪控制算法。
To study the attitude system of spacecraft, an adaptive inverse control algorithm is presented.
针对航天器姿态系统，提出了一种基于自适应神经网络动态逆的控制算法。
To study the attitude system of spacecraft, an adaptive inverse control algorithm is presented.
针对航天器姿态系统，提出了一种基于自适应神经网络动态逆的控制算法。
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