Development of Relative Degree-Based Aerospace Sliding Mode Control MATLAB Toolbox With Case Studies

被引：1
作者：
Kode, Sai Susheel Praneeth [1 ]
Shtessel, Yuri [1 ]
Levant, Arie [2 ]
Rakoczy, J. [3 ]
Hannan, M. [3 ]
Orr, J. [4 ]
机构：
[1] Univ Alabama Huntsville, Huntsville, AL 35899 USA
[2] Tel Aviv Univ, IL-69978 Tel Aviv, Israel
[3] Marshall Space Flight Ctr, NASA, Huntsville, AL 35801 USA
[4] Mclaurin Aerosp, Huntsville, AL 35804 USA
来源：
IEEE AEROSPACE AND ELECTRONIC SYSTEMS MAGAZINE | 2024年 / 39卷 / 09期
关键词：
Perturbation methods; Sliding mode control; Attitude control; Moon; Matlab; Aerospace and electronic systems; Aerodynamics; Autonomous aerial vehicles; Space vehicles; Aerospace engineering; Aerospace sliding mode control toolbox; relative degree; resource prospector lander; launch vehicle; ORDER; GUIDANCE; METHODOLOGY; ADAPTATION; TRACKING; DESIGN;
D O I：
10.1109/MAES.2022.3177576
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Sliding mode control and observation techniques are widely used in aerospace applications, including aircraft, UAVs, launch vehicles (LVs), missile interceptors, and hypersonic missiles. This work is dedicated to creating an MATLAB-based sliding mode controller design and simulation software toolbox that aims to support aerospace vehicle applications. An architecture of the aerospace sliding mode control toolbox (SMC Aero) using the relative degree approach is proposed. The SMC Aero libraries include first-order sliding mode control, second-order sliding mode control, and higher order sliding mode control (either fixed gain or adaptive), as well as higher order sliding mode differentiators. The efficacy of the SMC Aero toolbox is confirmed in two case studies: 1) controlling and 2) simulating resource prospector lander soft landing on the Moon and LV attitude control in ascent mode.
引用
收藏
页码：72 / 96
页数：25
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