Interception of the near space hypersonic weapons based on the partial integrated guidance and control method

DOI

10.2991/icmmita-16.2016.210How to use a DOI?

Keywords

Hypersonic target interception; high order sliding mode control; partial integrated guidance and control; arbitrary order robust exact differentiator.

Abstract

The interception of the hypersonic weapons in near space is the main problem considered in this paper. The designed interceptor is assumed to have much lower speed than its target and very limited maneuverability in the near space atmosphere. To deal with this problem, a two-loop Partial Integrated Guidance and Control (PIGC) scheme is introduced in this design. More specifically, an integrated full state feedback guidance loop and an inner state feedback control loop together provide a quick and stable response to the target maneuver. To realize the PIGC scheme, a Quasi-continuous High Order Sliding Mode controller is employed due to the high order relative degree nature of the PIGC model. Finally, numerical simulation results in three typical engagement scenarios are given to demonstrate the superiority of the proposed method.

Copyright

© 2017, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Bin Fu
AU  - Hang Guo
AU  - Jie Yan
PY  - 2017/01
DA  - 2017/01
TI  - Interception of the near space hypersonic weapons based on the partial integrated guidance and control method
BT  - Proceedings of the 2016 4th International Conference on Machinery, Materials and Information Technology Applications
PB  - Atlantis Press
SN  - 2352-538X
UR  - https://doi.org/10.2991/icmmita-16.2016.210
DO  - 10.2991/icmmita-16.2016.210
ID  - Fu2017/01
ER  -