Adaptive Disturbance-Based High-Order Sliding-Mode Control for Hypersonic-Entry Vehicles

Sagliano, Marco and Mooij, Erwin and Theil, Stephan (2017) Adaptive Disturbance-Based High-Order Sliding-Mode Control for Hypersonic-Entry Vehicles. Journal of Guidance, Control, and Dynamics, 40 (3), pp. 521-536. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.G000675 ISSN 0731-5090

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Official URL: http://dx.doi.org/10.2514/1.G000675

Item URL in elib:

https://elib.dlr.de/117119/

Document Type:

Article

Title:

Adaptive Disturbance-Based High-Order Sliding-Mode Control for Hypersonic-Entry Vehicles

Authors:

Authors	Institution or Email of Authors	Authors ORCID iD
Sagliano, Marco	Marco.Sagliano (at) dlr.de	https://orcid.org/0000-0003-1026-0693
Mooij, Erwin	e.mooij (at) tudelft.nl	UNSPECIFIED
Theil, Stephan	Stephan.Theil (at) dlr.de	https://orcid.org/0000-0002-5346-8091

Date:

March 2017

Journal or Publication Title:

Journal of Guidance, Control, and Dynamics

Refereed publication:

Yes

Open Access:

Yes

Gold Open Access:

In SCOPUS:

Yes

In ISI Web of Science:

Yes

Volume:

DOI :

10.2514/1.G000675

Page Range:

pp. 521-536

Publisher:

American Institute of Aeronautics and Astronautics (AIAA)

ISSN:

0731-5090

Status:

Published

Keywords:

Sliding Mode Theory, Atmospheric Entry, Nonlinear Control

HGF - Research field:

Aeronautics, Space and Transport

HGF - Program:

Space

HGF - Program Themes:

Space Transport

DLR - Research area:

Raumfahrt

DLR - Program:

R RP - Raumtransport

DLR - Research theme (Project):

R - Shefex III

Location:

Bremen

Institutes and Institutions:

Institute of Space Systems > Navigation and Control Systems

Deposited By:

Sagliano, Marco

Deposited On:

13 Dec 2017 10:46

Last Modified:

31 Jul 2019 20:14

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