Waypoints Following Guidance for Surface-to-Surface Missiles

Hao Zhou; Elsayed M. Khalil; Tawfiqur Rahman; Wanchun Chen

doi:10.1007/s42405-018-0007-5

Waypoints Following Guidance for Surface-to-Surface Missiles

Hao Zhou^*
, Elsayed M. Khalil
, Tawfiqur Rahman
, Wanchun Chen

^*Corresponding author for this work

School of Astronautics

Beihang University
Directorate of Engineering

Research output: Contribution to journal › Article › peer-review

1 Scopus citations

Abstract

The paper proposes waypoints following guidance law. In this method an optimal trajectory is first generated which is then represented through a set of waypoints that are distributed from the starting point up to the final target point using a polynomial. The guidance system then works by issuing guidance command needed to move from one waypoint to the next one. Here the method is applied for a surface-to-surface missile. The results show that the method is feasible for on-board application.

Original language	English
Pages (from-to)	183-195
Number of pages	13
Journal	International Journal of Aeronautical and Space Sciences
Volume	19
Issue number	1
DOIs	https://doi.org/10.1007/s42405-018-0007-5
State	Published - 1 Mar 2018

Keywords

Inverse dynamic guidance
Missile guidance
Surface-to-surface missile
Waypoints following guidance

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10.1007/s42405-018-0007-5

Cite this

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title = "Waypoints Following Guidance for Surface-to-Surface Missiles",

abstract = "The paper proposes waypoints following guidance law. In this method an optimal trajectory is first generated which is then represented through a set of waypoints that are distributed from the starting point up to the final target point using a polynomial. The guidance system then works by issuing guidance command needed to move from one waypoint to the next one. Here the method is applied for a surface-to-surface missile. The results show that the method is feasible for on-board application.",

keywords = "Inverse dynamic guidance, Missile guidance, Surface-to-surface missile, Waypoints following guidance",

author = "Hao Zhou and Khalil, \{Elsayed M.\} and Tawfiqur Rahman and Wanchun Chen",

note = "Publisher Copyright: {\textcopyright} 2018, The Korean Society for Aeronautical \& Space Sciences and Springer Nature Singapore Pte Ltd.",

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doi = "10.1007/s42405-018-0007-5",

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AU - Khalil, Elsayed M.

AU - Rahman, Tawfiqur

AU - Chen, Wanchun

PY - 2018/3/1

Y1 - 2018/3/1

N2 - The paper proposes waypoints following guidance law. In this method an optimal trajectory is first generated which is then represented through a set of waypoints that are distributed from the starting point up to the final target point using a polynomial. The guidance system then works by issuing guidance command needed to move from one waypoint to the next one. Here the method is applied for a surface-to-surface missile. The results show that the method is feasible for on-board application.

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KW - Missile guidance

KW - Surface-to-surface missile

KW - Waypoints following guidance

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Waypoints Following Guidance for Surface-to-Surface Missiles

Abstract

Keywords

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