Halo orbit targeting guidance via higher order sliding techniques

Jules Simo; Roberto Fufaro; Daniel Wibben

Halo orbit targeting guidance via higher order sliding techniques

Jules Simo, Roberto Fufaro, Daniel Wibben

Mechanical And Aerospace Engineering

Research output: Chapter in Book/Report/Conference proceeding › Chapter (peer-reviewed)

42 Downloads (Pure)

Abstract

In this paper, the Multiple Sliding Surface Guidance (MSSG) algorithm has been implemented and simulated to verify the ability to target the insertion point of a suitable halo orbit in the vicinity of the Sun-Earth libration points. Based on Higher-Order Sliding Control (HOSC) theory, the proposed MSSG algorithm computes an acceleration command that target a specified state by considering only knowledge of the current and desired position and velocity. Results show that the guidance scheme is able to successfully target a suitable state for proper orbital insertion. Furthermore, it will be shown how the algorithm can be used to target the L1 point in the Sun-Earth system. A detailed study has also been performed to investigate the guidance performances as function of the guidance parameters. The global stability of the proposed guidance scheme is proven using Lyapunov-based approach.

Original language	English
Title of host publication	Advances in Astronautical Sciences
Subtitle of host publication	Astrodynamics 2013
Editors	Stephen B. Broschart, James D. Turner, Kathleen Howell, Felix Hoots
Place of Publication	Hilton Head SC
Pages	2341-2354
Number of pages	14
Volume	150
Publication status	Published - 11 Aug 2013
Event	AAS/AIAA Astrodynamics Specialist Conference 2013 - Hilton Head, South Carolina, United States Duration: 11 Aug 2013 → 15 Aug 2013

Publication series

Name	Advances in the Astronautical Sciences
Publisher	Univelt
Number	I-III
Volume	150

Conference

Conference	AAS/AIAA Astrodynamics Specialist Conference 2013
Country	United States
City	Hilton Head, South Carolina
Period	11/08/13 → 15/08/13

Keywords

halo orbit
guidance control systems
sliding mode control

Access to Document

Simo-J-et-al-Astrodyn-Spec-Conf-Halo-orbit-targeting-guidance-higher-order-sliding-techniques-2013Accepted author manuscript, 513 KB

http://www.univelt.com/book=4275

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Simo, J., Fufaro, R., & Wibben, D. (2013). Halo orbit targeting guidance via higher order sliding techniques. In S. B. Broschart, J. D. Turner, K. Howell, & F. Hoots (Eds.), Advances in Astronautical Sciences: Astrodynamics 2013 (Vol. 150, pp. 2341-2354). [AAS 13-860] (Advances in the Astronautical Sciences; Vol. 150, No. I-III). Hilton Head SC.

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abstract = "In this paper, the Multiple Sliding Surface Guidance (MSSG) algorithm has been implemented and simulated to verify the ability to target the insertion point of a suitable halo orbit in the vicinity of the Sun-Earth libration points. Based on Higher-Order Sliding Control (HOSC) theory, the proposed MSSG algorithm computes an acceleration command that target a specified state by considering only knowledge of the current and desired position and velocity. Results show that the guidance scheme is able to successfully target a suitable state for proper orbital insertion. Furthermore, it will be shown how the algorithm can be used to target the L1 point in the Sun-Earth system. A detailed study has also been performed to investigate the guidance performances as function of the guidance parameters. The global stability of the proposed guidance scheme is proven using Lyapunov-based approach.",

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author = "Jules Simo and Roberto Fufaro and Daniel Wibben",

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language = "English",

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Simo, J, Fufaro, R & Wibben, D 2013, Halo orbit targeting guidance via higher order sliding techniques. in SB Broschart, JD Turner, K Howell & F Hoots (eds), Advances in Astronautical Sciences: Astrodynamics 2013. vol. 150, AAS 13-860, Advances in the Astronautical Sciences, no. I-III, vol. 150, Hilton Head SC, pp. 2341-2354, AAS/AIAA Astrodynamics Specialist Conference 2013, Hilton Head, South Carolina, United States, 11/08/13.

Halo orbit targeting guidance via higher order sliding techniques. / Simo, Jules; Fufaro, Roberto; Wibben, Daniel.

Advances in Astronautical Sciences: Astrodynamics 2013. ed. / Stephen B. Broschart; James D. Turner; Kathleen Howell; Felix Hoots. Vol. 150 Hilton Head SC, 2013. p. 2341-2354 AAS 13-860 (Advances in the Astronautical Sciences; Vol. 150, No. I-III).

Research output: Chapter in Book/Report/Conference proceeding › Chapter (peer-reviewed)

TY - CHAP

T1 - Halo orbit targeting guidance via higher order sliding techniques

AU - Simo, Jules

AU - Fufaro, Roberto

AU - Wibben, Daniel

PY - 2013/8/11

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N2 - In this paper, the Multiple Sliding Surface Guidance (MSSG) algorithm has been implemented and simulated to verify the ability to target the insertion point of a suitable halo orbit in the vicinity of the Sun-Earth libration points. Based on Higher-Order Sliding Control (HOSC) theory, the proposed MSSG algorithm computes an acceleration command that target a specified state by considering only knowledge of the current and desired position and velocity. Results show that the guidance scheme is able to successfully target a suitable state for proper orbital insertion. Furthermore, it will be shown how the algorithm can be used to target the L1 point in the Sun-Earth system. A detailed study has also been performed to investigate the guidance performances as function of the guidance parameters. The global stability of the proposed guidance scheme is proven using Lyapunov-based approach.

AB - In this paper, the Multiple Sliding Surface Guidance (MSSG) algorithm has been implemented and simulated to verify the ability to target the insertion point of a suitable halo orbit in the vicinity of the Sun-Earth libration points. Based on Higher-Order Sliding Control (HOSC) theory, the proposed MSSG algorithm computes an acceleration command that target a specified state by considering only knowledge of the current and desired position and velocity. Results show that the guidance scheme is able to successfully target a suitable state for proper orbital insertion. Furthermore, it will be shown how the algorithm can be used to target the L1 point in the Sun-Earth system. A detailed study has also been performed to investigate the guidance performances as function of the guidance parameters. The global stability of the proposed guidance scheme is proven using Lyapunov-based approach.

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