【摘要】：在入軌段測(cè)控任務(wù)中,為了實(shí)時(shí)監(jiān)視火箭和衛(wèi)星的天線方向性,基于測(cè)量船跟蹤計(jì)算軟件的實(shí)際,通過分析入軌段火箭飛行姿態(tài)、位侕等測(cè)量數(shù)據(jù),設(shè)計(jì)利用火箭實(shí)時(shí)遙測(cè)數(shù)據(jù)計(jì)算火箭和衛(wèi)星天線方向性的方案,規(guī)定了具體流程,并通過實(shí)例計(jì)算,驗(yàn)證了該方法的可行性。
[Abstract]:In order to monitor the antenna directivity of rocket and satellite in real time, based on the reality of the tracking calculation software of the measuring ship, the scheme of calculating the directivity of rocket and satellite antenna by using rocket real-time telemetry data is designed by analyzing the flight attitude and position measurement data of the rocket in the orbital section, and the feasibility of the method is verified by an example calculation.
【作者單位】： 中國(guó)衛(wèi)星海上測(cè)控部;
【分類號(hào)】：V556
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本文編號(hào)：2525327