Title: Full-distance inertial guidance trajectory technique for ground to ground missile
Abstract: Design principle of full-distance inertial guidance trajectory for ground to ground missile in range of 150~250 km was analyzed by means of proportional guide trajectory theory and simulation calculation.The trajectory features consist of four characteristic points,such as flameout point,turning point,dive point and target point.The range of missile can be changed by adjustment of three parameters(turning point,dive point and target point).Function and selection principle of four characteristic points were given through trajectory simulation investigation.Advantages and disadvantages of full-distance trajectory control scheme were analyzed.
Publication Year: 2007
Publication Date: 2007-01-01
Language: en
Type: article
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