Three-dimensional terminal angle constraint guidance law with class K∞ function-based adaptive sliding mode control
This paper investigates the three-dimensional (3-D) interception guidance problem, where the missile is required to intercept the maneuvering target with the desired terminal angles. For the nonlinear relative kinematic model, a class K∞ function-based adaptive sliding mode guidance law is proposed,...
Saved in:
Main Authors: | Zheng, Zewei, Li, Jiazhe, Feroskhan, Mir |
---|---|
Other Authors: | School of Mechanical and Aerospace Engineering |
Format: | Article |
Language: | English |
Published: |
2024
|
Subjects: | |
Online Access: | https://hdl.handle.net/10356/176061 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Nanyang Technological University |
Language: | English |
Similar Items
-
A discrete-time terminal sliding-mode control approach applied to a motion control problem
by: Abidi, K., et al.
Published: (2014) -
Sliding Mode Control: The Delta-Sigma Modulation Approach
by: Hu, Hesuan
Published: (2017) -
Development and applications of new sliding mode control approaches
by: PAN YAJUN
Published: (2010) -
A quasi-tracking approach for finite-time control of a mass-beam system
by: Zhu, G., et al.
Published: (2014) -
Sliding-mode-observer-based adaptive slip ratio control for electric and hybrid vehicles
by: Subudhi, B., et al.
Published: (2014)