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

Sai Susheel Praneeth Kode; Yuri Shtessel; Arie Levant; J. Rakoczy; M. Hannan; J. Orr

doi:10.1109/MAES.2022.3177576

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

Sai Susheel Praneeth Kode, Yuri Shtessel, Arie Levant, J. Rakoczy, M. Hannan, J. Orr

School of Mathematical Sciences

Tel Aviv University

Research output: Contribution to journal › Article › peer-review

Abstract

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.

Original language	English
Pages (from-to)	72-96
Number of pages	25
Journal	IEEE Aerospace and Electronic Systems Magazine
Volume	39
Issue number	9
DOIs	https://doi.org/10.1109/MAES.2022.3177576
State	Published - 2024

Keywords

Aerospace sliding mode control toolbox
launch vehicle
relative degree
resource prospector lander

All Science Journal Classification (ASJC) codes

Aerospace Engineering
Space and Planetary Science
Electrical and Electronic Engineering

Access to Document

10.1109/MAES.2022.3177576

Cite this

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title = "Development of Relative Degree-Based Aerospace Sliding Mode Control MATLAB Toolbox With Case Studies",

abstract = "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.",

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author = "Kode, {Sai Susheel Praneeth} and Yuri Shtessel and Arie Levant and J. Rakoczy and M. Hannan and J. Orr",

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doi = "10.1109/MAES.2022.3177576",

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AU - Hannan, M.

AU - Orr, J.

PY - 2024

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AB - 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.

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JO - IEEE Aerospace and Electronic Systems Magazine

JF - IEEE Aerospace and Electronic Systems Magazine

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

Abstract

Keywords

All Science Journal Classification (ASJC) codes

Access to Document

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