Design and Simulation of Finite-time Convergence with Impact angle constraint Sliding-mode Guidance Law

DOI

10.2991/icamcs-16.2016.167How to use a DOI?

Keywords

Impact angle constraint,Finite-time convergence, Sliding-mode guidance law,

Abstract

For missile falling angle constraint targets to prevent target evasive maneuvers, missile target relative motion relationship is established, based on the sliding mode variable structure theory, the linear sliding surface, select adaptive power reaching law is proposed with the drop angle constraint of sliding mode guidance law. By using Lyapunov theory guidance law of stability analysis, the analysis of the guidance law with finite time convergence. Simulation results show that the designed guidance law is compared to the traditional guidance law, the performance is more superior, has strong robustness, meet the design requirements.

Copyright

© 2016, 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  - Kai Zhang
AU  - Suo-chang Yang
AU  - Kuan-qiao Zhang
AU  - Yun-zhi Yao
AU  - Peng Chen
PY  - 2016/06
DA  - 2016/06
TI  - Design and Simulation of Finite-time Convergence with Impact angle constraint Sliding-mode Guidance Law
BT  - Proceedings of the 2016 5th International Conference on Advanced Materials and Computer Science
PB  - Atlantis Press
SP  - 818
EP  - 824
SN  - 2352-5401
UR  - https://doi.org/10.2991/icamcs-16.2016.167
DO  - 10.2991/icamcs-16.2016.167
ID  - Zhang2016/06
ER  -