Adaptive Sliding Mode Guidance Law with Terminal Angle Constraint
- 10.2991/lemcs-15.2015.155How to use a DOI?
- Guidance law; Terminal angle constraint; Sliding mode variable structure; Relative velocity deflection angle; Adaptive reaching law
As it is important to attack the targets with terminal angle constraint for a lot of guided weapons, an adaptive sliding mode guidance law is proposed based on the sliding mode variable structure control theory. Considering the problems that the terminal line of sight angle speed changes rapidly and terminal angle constraint, the guidance law chooses relative velocity deflection angle as the sliding mode surface, introduces terminal angle constraint, regards the target maneuvering as limited disturbance, and uses Lyapunov stability theory to analyze the stability of the guidance law. In order to weaken the chattering phenomenon of variable structure control, the guidance law proposes a new method that combining the variable switch term with saturated function. Finally, the designed guidance law is applied to the missile actual model to make a contrastive simulation, the results show that compared with the traditional method, the proposed guidance law can attack the target with less miss distance and terminal angle error, and has strong robustness.
- © 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 - Kuanqiao Zhang AU - Suochang Yang PY - 2015/07 DA - 2015/07 TI - Adaptive Sliding Mode Guidance Law with Terminal Angle Constraint BT - Proceedings of the International Conference on Logistics, Engineering, Management and Computer Science PB - Atlantis Press SP - 792 EP - 796 SN - 1951-6851 UR - https://doi.org/10.2991/lemcs-15.2015.155 DO - 10.2991/lemcs-15.2015.155 ID - Zhang2015/07 ER -