Robust Control Compensation for Space Descent and Landing

Pedro Simplicio; Andres Marcos; Eric Joffre; Mattia Zamaro; Nuno Silva

doi:10.23919/ECC.2018.8550147

Robust Control Compensation for Space Descent and Landing

Pedro Simplicio, Andres Marcos, Eric Joffre, Mattia Zamaro, Nuno Silva

Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

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Abstract

This paper presents a complete modelling, synthesis and analysis methodology of control compensators for descent and landing on small planetary bodies. These missions are scientifically very rewarding, but also extremely challenging due to the complex and poorly-known environment around those bodies, calling for the ability to manage competing robustness/performance requirements by design. Here, this is achieved using robust control tools and the recently-developed structured H∞ framework. The proposed method is verified for three distinct landing trajectories on the Martian moon Phobos.

Original language	English
Title of host publication	2018 European Control Conference (ECC 2018)
Subtitle of host publication	Proceedings of a meeting held 12-15 June 2018, Limassol, Cyprus
Publisher	Institute of Electrical and Electronics Engineers (IEEE)
Pages	155-160
Number of pages	6
ISBN (Electronic)	9783952426982
ISBN (Print)	9781538653036
DOIs	https://doi.org/10.23919/ECC.2018.8550147
Publication status	Published - Dec 2018
Event	17th European Control Conference - Duration: 12 Jun 2018 → 15 Jun 2018 http://www.ecc18.eu/

Conference

Conference	17th European Control Conference
Abbreviated title	ECC 2018
Period	12/06/18 → 15/06/18
Internet address	http://www.ecc18.eu/

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10.23919/ECC.2018.8550147

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Robust and Nonlinear Guidance & Control for Landing on Small Bodies
Simplicio, P. V. M. (Principal Investigator) & Marcos, A. (Principal Investigator)
1/04/16 → 1/04/17
Project: Research

Cite this

@inproceedings{36c1bd9bf1e141af868453ab81935f27,

title = "Robust Control Compensation for Space Descent and Landing",

abstract = "This paper presents a complete modelling, synthesis and analysis methodology of control compensators for descent and landing on small planetary bodies. These missions are scientifically very rewarding, but also extremely challenging due to the complex and poorly-known environment around those bodies, calling for the ability to manage competing robustness/performance requirements by design. Here, this is achieved using robust control tools and the recently-developed structured H∞ framework. The proposed method is verified for three distinct landing trajectories on the Martian moon Phobos.",

author = "Pedro Simplicio and Andres Marcos and Eric Joffre and Mattia Zamaro and Nuno Silva",

year = "2018",

month = dec,

doi = "10.23919/ECC.2018.8550147",

language = "English",

isbn = "9781538653036",

pages = "155--160",

booktitle = "2018 European Control Conference (ECC 2018)",

publisher = "Institute of Electrical and Electronics Engineers (IEEE)",

address = "United States",

note = "17th European Control Conference, ECC 2018 ; Conference date: 12-06-2018 Through 15-06-2018",

url = "http://www.ecc18.eu/",

}

Simplicio, P, Marcos, A, Joffre, E, Zamaro, M & Silva, N 2018, Robust Control Compensation for Space Descent and Landing. in 2018 European Control Conference (ECC 2018): Proceedings of a meeting held 12-15 June 2018, Limassol, Cyprus. Institute of Electrical and Electronics Engineers (IEEE), pp. 155-160, 17th European Control Conference, 12/06/18. https://doi.org/10.23919/ECC.2018.8550147

Robust Control Compensation for Space Descent and Landing. / Simplicio, Pedro; Marcos, Andres; Joffre, Eric et al.
2018 European Control Conference (ECC 2018): Proceedings of a meeting held 12-15 June 2018, Limassol, Cyprus. Institute of Electrical and Electronics Engineers (IEEE), 2018. p. 155-160.

Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

TY - GEN

T1 - Robust Control Compensation for Space Descent and Landing

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AU - Marcos, Andres

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AU - Zamaro, Mattia

AU - Silva, Nuno

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Y1 - 2018/12

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AB - This paper presents a complete modelling, synthesis and analysis methodology of control compensators for descent and landing on small planetary bodies. These missions are scientifically very rewarding, but also extremely challenging due to the complex and poorly-known environment around those bodies, calling for the ability to manage competing robustness/performance requirements by design. Here, this is achieved using robust control tools and the recently-developed structured H∞ framework. The proposed method is verified for three distinct landing trajectories on the Martian moon Phobos.

U2 - 10.23919/ECC.2018.8550147

DO - 10.23919/ECC.2018.8550147

M3 - Conference Contribution (Conference Proceeding)

SN - 9781538653036

SP - 155

EP - 160

BT - 2018 European Control Conference (ECC 2018)

PB - Institute of Electrical and Electronics Engineers (IEEE)

T2 - 17th European Control Conference

Y2 - 12 June 2018 through 15 June 2018

ER -

Robust Control Compensation for Space Descent and Landing

Abstract

Conference

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Projects

Robust and Nonlinear Guidance & Control for Landing on Small Bodies

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