Research on Trajectory Scheme with Large Impact Angle for Fire-and-Forget Anti-Tank Missiles

DOI

10.2991/asei-15.2015.235How to use a DOI?

Keywords

anti-tank missile, angle constraints, guidance law , autopilot.

Abstract

In order to achieve the damage effect, when the anti-tank missile hits the target in the top attack model, both precision and terminal impact angle should be satisfied. Firstly, a kind of proportional navigation law with impact position and angle constraint was deduced. Then, the top attack trajectory of the anti-tank missile was designed, the missile flies out of the tube without control, the climb stage was completed by the index number regulation, the stage of glide at a certain angle of attack, at the end of the trajectory the guidance law which was deduced was adopted to satisfy the impact position and angular constraint. The required autopilots were also designed. The results of simulation showed that the trajectory scheme has strong effectiveness for the anti-tank missile to attack targets at different range.

Copyright

© 2015, 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  - Wendong Zhao
AU  - Min Gao
AU  - Wei Huang
AU  - Huimin Wang
PY  - 2015/05
DA  - 2015/05
TI  - Research on Trajectory Scheme with Large Impact Angle for Fire-and-Forget Anti-Tank Missiles
BT  - Proceedings of the 2015 International conference on Applied Science and Engineering Innovation
PB  - Atlantis Press
SP  - 1187
EP  - 1191
SN  - 2352-5401
UR  - https://doi.org/10.2991/asei-15.2015.235
DO  - 10.2991/asei-15.2015.235
ID  - Zhao2015/05
ER  -