Bezier-curve navigation guidance for impact time and angle control

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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, and always exists in the convex hull of the control points. Proposed Bézier curve navigation guidance, makes the missile follow the Bézier curve with the feedback form of guidance command so that the missile hits the target on the desired time in the desired direction. We conducted numerical simulations on several terminal conditions to demonstrate the performance of proposed method. © 2018. Published by INCAS.
Publisher
INCAS - National Institute for Aerospace Research Elie Carafoli
Issue Date
2018
Language
English
Article Type
Article
Citation

INCAS Bulletin, v.10, no.1, pp.105 - 115

ISSN
2066-8201
DOI
10.13111/2066-8201.2018.10.1.11
URI
http://hdl.handle.net/10203/248797
Appears in Collection
AE-Journal Papers(저널논문)
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