一种卫星通信载波滚转角控制算法

Wei Zhang, Na Meng, Shaoft Zhang, Wei Wang
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引用次数: 0

摘要

为了保证卫星通信链路的稳定性,必须保证载波上通信终端的天线实时指向通信卫星。然而,载波姿态的剧烈变化可能导致通信终端天线无法准确指向卫星,最终导致卫星通信链路中断。为了解决这一问题,本文提出了一种载波横摇角控制算法。首先,假设载体的横摇角为0°。然后,根据载体的位置(经度、纬度、高度)和姿态(俯仰、偏航、横摇),计算天线指向通信卫星的角度,得到方向角在载体横截面上的投影。最后,该投影与上述载体方向的夹角为最优横摇角。在载波姿态和位置不变的情况下,该最优滚转角可以使天线指向通信卫星的角度最小,从而最大限度地获得天线增益,极大地提高卫星通信性能。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A Carrier Roll Angle Control Algorithm for Satellite Communication
In order to ensure the stability of the satellite communication link, it is necessary to ensure that the antenna of the communication terminal on the carrier directs to the communication satellite in real time.However, the drastic changes of the carrier attitude may cause the antenna of the communication terminal cannot direct to satellite accurately, which resulting the interruption of satellite communication link finally. To solve the problem, a carrier roll angle control algorithm is proposed in this paper. Firstly, it is assumed that the roll angle of the carrier is 0°. Then, according to the position(longitude, latitude, altitude)and the attitude(pitch, yaw, roll) of the carrier, the angle of the antenna directing to communication satellite is calculated and the projection of the direction angle on the cross section of the carrier is obtained. Finally, the included angle of this projection and the above direction of carrier is the optimal roll angle. When the attitude and the position of the carrier are unchanged, this optimal roll angle can make the angle of the antenna directing to communication satellite to be minimized, thus to obtain the antenna gain maximally and improve the performance of satellite communication greatly.
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