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The comparison of attitude and antenna pointing design strategies of noncooperative spaceborne bistatic radar

机译:非合作星载双基地雷达姿态和天线指向设计策略的比较

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Satellite attitude and antenna pointing design strategy is the key design issue of distributed spaceborne radar system design. In the case of noncooperative transmitter, the article presents six attitude and antenna pointing parameter strategies. Several mathematic methods are provided as follows. A general method of beam-pointing synchronization is summarized. Six methods of beam synchronization are provided, each corresponding to one of six attitude and antenna pointing strategies above. An approach of how to compute the requirement of control ability of attitude and antenna pointing is presented. In order to compare with performance of six parameter strategies, a swath overlap ability model is put forward. Lastly, a simulation case is presented, in which attitude and antenna pointing angles and swath overlap abilities of six parameter strategies are compared with each other. The simulation results prove correctness and validity of design methods.
机译:卫星姿态和天线指向设计策略是分布式星载雷达系统设计的关键设计问题。对于不合作的发射机,本文提出了六种姿态和天线指向参数策略。以下提供了几种数学方法。总结了一种波束指向同步的通用方法。提供了六种波束同步方法,每种方法都对应于上述六个姿态和天线指向策略之一。提出了一种计算姿态和天线指向控制能力要求的方法。为了与六参数策略的性能进行比较,提出了条带重叠能力模型。最后,给出了一个仿真案例,其中将姿态和天线指向角以及六个参数策略的条带重叠能力进行了比较。仿真结果证明了设计方法的正确性和有效性。

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