計測自動制御学会論文集
Online ISSN : 1883-8189
Print ISSN : 0453-4654
ISSN-L : 0453-4654
誘導飛翔体に搭載された目標追尾装置の空間安定特性
評価とその応用
江口 弘文渡辺 憲司山下 忠
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ジャーナル フリー

1989 年 25 巻 11 号 p. 1186-1193

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抄録
A guided vehicle which utilizes the principle of proportional navigation has a target tracker to measure the angular rate of the line-of-sight. This tracker consists of 2-axes gimbals mechanisms to prevent the “tracker-to-vehicle” coupling. But no gimbals mechanisms have perfect performance, and as well known in the practical guidance system designer, the “tracker-to-vehicle” coupling suppresses the guidance system performance.
This paper presents a definition and a mathematical model of the “tracker-to-vehicle” coupling. Then, by using the definition and the model, the constraint conditions of the “tracker-to-vehicle” coupling for a target tracker are shown by two methods. The first is by the stability analyses of the parasitic loop which are generated by the existence of the “tracker-to-vehicle” coupling. The second is by the simulation analysis of the guidance system including “tracker-to-vehicle” coupling.
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© 社団法人 計測自動制御学会
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