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Asynchronous Guidance Filter Design Based On Strapdown Seeker And Ins Information

JOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES(2020)

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摘要
In this paper, we propose a guidance filter to estimate line of sight rate with strapdown seeker measurements and INS(Inertial Navigation System) information. The measurements of proposed guidance filter consisted of the LOS(Line of Sight) and relative position that can be calculated with the seeker's measurements, INS information and known target position, also the filter is based on an asynchronous filter to use outputs of the two sensors that are out of synchronous and period. Through the proposed filter, we can reduce the effect on parasitic loop that can be caused by using large time delay seeker and improve the estimation performance.
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关键词
Guidance Filter, Asynchronous Filter, Strapdown Seeker, Line of Sight Rate Estimation, Sensor Fusion, Parasitic Loop
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