Research on Trajectory Scheme with Large Impact Angle for Fire-and-Forget Anti-Tank Missiles
- 10.2991/asei-15.2015.235How to use a DOI?
- anti-tank missile, angle constraints, guidance law , autopilot.
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.
- © 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/).
Cite this article
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 -