The Design of the Best Penetration Maneuvers Parameter of Variable Trajectory Maneuvers of Target Missiles
- DOI
- 10.2991/msota-16.2016.49How to use a DOI?
- Keywords
- target missile; variable trajectory maneuvers; penetration effect formatting
- Abstract
To solve the design problem of variable trajectory maneuver of target missiles, an integrated design model of variable trajectory maneuver is presented. By closely cooperating between the control signals of displacements and the control signals of overloads, this integrated design model can make target missiles to realize the maneuver of jump trajectory, the maneuver of snake-wriggling trajectory, the maneuver of pendulum trajectory, the maneuver of spiral trajectory, and so on. On this basis, the penetration effect models of variable trajectory maneuvers of target missiles are researched. The design methods of the best penetration maneuvers parameter is put forward. According to the analysis, target missiles should enlarge maneuver amplitude Ay and Az as much as possible within the overload limit. At the same time, we select the optimal parameter kyopt and kzopt according to various maneuver modes. According to these parameters, variable trajectory maneuver of target missiles can realize the best penetration effect, and promote train effect of air defense missile.
- 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/).
Cite this article
TY - CONF AU - Kaibo Bi AU - Yifei Zhang AU - Xianhui Sui PY - 2016/12 DA - 2016/12 TI - The Design of the Best Penetration Maneuvers Parameter of Variable Trajectory Maneuvers of Target Missiles BT - Proceedings of 2016 International Conference on Modeling, Simulation and Optimization Technologies and Applications (MSOTA2016) PB - Atlantis Press SP - 218 EP - 224 SN - 2352-538X UR - https://doi.org/10.2991/msota-16.2016.49 DO - 10.2991/msota-16.2016.49 ID - Bi2016/12 ER -