Design of Longitudinal Landing Control Law Based on Terminal Sliding Mode in Simplified Model
LI Zexue
Abstract：This paper presents an integrated Terminal sliding mode control method that is proposed to control the attitude of carrier-based aircraft during landing. The stability of the system is analyzed according to Lyapunov stability theory and the system is simulated by Matlab/Simulink. The simulation results show that the designed longitudinal landing control law has the ability to re?strain uncertainty and interference,and it can control the longitudinal attitude of the carrier-based aircraft.
Keywords：Terminal sliding mode controlLyapunov stabilitycarrier-based aircraftautomatic landing control system
Publication Date：2019-01-01
Online Publishing Date：2025-08-15(First online date of this platform, not the publication date of the document)
Pages：4( 63-66 )