Bezier-curve Navigation Guidance for Impact Time and Angle Control

This paper addresses a novel impact time and angle control guidance law using a Bézier curve. The 2nd order Bézier curve consists of one control point and two boundary points; initial point P0, middle point P1 and end point P2. The curve is tangent to the line P0-P1 and the line P1-P2, respectively,...

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Bibliographic Details
Main Authors: Gun-Hee MOON, Sang-Wook SHIM, Min-Jea TAHK
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2018-03-01
Series:INCAS Bulletin
Subjects:
Online Access:http://bulletin.incas.ro/files/moon_shim_tahk_vol_10_iss_1.pdf