Instrument Landing System Lateral Beam Guidance System Based on Sliding Mode Control Technique
En este artículo se muestra un entorno basado en Matlab-Simulink para el análisis de un sistema de aterrizaje de un avión que puede ser utilizado para el aterrizaje automatizado o asistido. Se describe la construcción de un modelo matemático que posteriormente es simulado para validar su funcionamie...
Main Authors: | Alejandro Paul Gomez, Juan Francisco Sotomayor |
---|---|
Format: | Article |
Language: | Spanish |
Published: |
Escuela Politécnica Nacional (EPN)
2014-02-01
|
Series: | Revista Politécnica |
Online Access: | https://revistapolitecnica.epn.edu.ec/ojs2/index.php/revista_politecnica2/article/view/111 |
Similar Items
-
Backstepping Sliding Mode Control for Radar Seeker Servo System Considering Guidance and Control System
by: Yexing Wang, et al.
Published: (2018-09-01) -
Integrated Aircraft Robust Output Feedback Sliding Mode Autopilot and Guidance System Design
by: Chang, Tzu-Yin, et al.
Published: (2012) -
Guidance Law Design: Sliding Mode Control Approach
by: Hao-Ting Chiang, et al.
Published: (2006) -
Sliding Mode Control Based Guidance Strategies with Terminal Constraints
by: Kumar, Shashi Ranjan
Published: (2018) -
Adaptive Sliding Mode Guidance With Impact Time and Angle Constraints
by: Xiaodong Liu, et al.
Published: (2020-01-01)