从编队内战术通信系统的基本要求出发,分析了发展舰载FSO(Free Space Optical)通信系统用于舰艇内部战术通信的优势。研究了舰载FSO通信系统的组成,以及实际作战应用时的网络拓扑结构。根据国际国内已有FSO技术的发展现状,研究了现有FS...从编队内战术通信系统的基本要求出发,分析了发展舰载FSO(Free Space Optical)通信系统用于舰艇内部战术通信的优势。研究了舰载FSO通信系统的组成,以及实际作战应用时的网络拓扑结构。根据国际国内已有FSO技术的发展现状,研究了现有FSO技术用于舰载FSO通信系统需解决的背景光干扰、大气传输效应等关键问题,分析了大气湍流强度、传输距离、激光波长和激光通信系统误码率之间的定量关系,最后提出下一步的研究重点。展开更多
In this paper, two formation controllers are developed under directed and undirected communication topology for six-degree-of-freedom （6-DOF） networked spacecraft flying in deep space. In the control algorithm, any ...In this paper, two formation controllers are developed under directed and undirected communication topology for six-degree-of-freedom （6-DOF） networked spacecraft flying in deep space. In the control algorithm, any explicit leader does not exist in the formation team and the proposed controller is required that each spacecraft communicates with its neighbors only, which avoids having to communicate each spacecraft＇s trajectory and therefore reduces the required communication loads of the whole formation. The proposed control strategy allows that each spacecraft can track its desired position and attitude and simultaneously the whole group moves to the desired formation and obtains its desired relative attitudes between spaceerafts. Simulation results demonstrate the effectiveness of the proposed controller.展开更多
文摘从编队内战术通信系统的基本要求出发,分析了发展舰载FSO(Free Space Optical)通信系统用于舰艇内部战术通信的优势。研究了舰载FSO通信系统的组成,以及实际作战应用时的网络拓扑结构。根据国际国内已有FSO技术的发展现状,研究了现有FSO技术用于舰载FSO通信系统需解决的背景光干扰、大气传输效应等关键问题,分析了大气湍流强度、传输距离、激光波长和激光通信系统误码率之间的定量关系,最后提出下一步的研究重点。
基金Supported by the National Natural Science Foundation of China （No. 10832004）.
文摘In this paper, two formation controllers are developed under directed and undirected communication topology for six-degree-of-freedom （6-DOF） networked spacecraft flying in deep space. In the control algorithm, any explicit leader does not exist in the formation team and the proposed controller is required that each spacecraft communicates with its neighbors only, which avoids having to communicate each spacecraft＇s trajectory and therefore reduces the required communication loads of the whole formation. The proposed control strategy allows that each spacecraft can track its desired position and attitude and simultaneously the whole group moves to the desired formation and obtains its desired relative attitudes between spaceerafts. Simulation results demonstrate the effectiveness of the proposed controller.
