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23976

DESIGN OF THE GUIDANCE, NAVIGATION AND CONTROL SYSTEM OF A LUNAR LANDER

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Last updated: 04 Jan 2025

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Abstract

ABSTRACT
This paper provides the MDLM (Moon Descent Landing Module) Guidance, Navigation and Control system design description as result of the analysis and trade-off performed in the frame of the “Italian Vision for Moon Exploration" studies of the Italian Space Agency (ASI). The preliminary design of the GNC system for the lunar lander was performed following the analysis of mission and the design requisites, the definition of the RCS architecture, the simulation of system performances, and, finally, the hardware and the equipments.

DOI

10.21608/asat.2007.23976

Keywords

Spacecraft Dynamics, guidance, Navigation and Control, Space Exploration

Authors

First Name

GUGLIERI

Last Name

G.

MiddleName

-

Affiliation

Politecnico di Torino, Dipartimento di Ingegneria Aeronautica e Spaziale, Torino, Italy.

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First Name

PERINO

Last Name

A.

MiddleName

M.

Affiliation

Alcatel Alenia Space, Torino, Italy.

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Orcid

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First Name

QUAGLIOTTI

Last Name

F.

MiddleName

-

Affiliation

Politecnico di Torino, Dipartimento di Ingegneria Aeronautica e Spaziale, Torino, Italy.

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Volume

12

Article Issue

ASAT Conference, 29-31 May 2007

Related Issue

4431

Issue Date

2007-05-01

Receive Date

2019-01-09

Publish Date

2007-05-01

Page Start

1

Page End

17

Print ISSN

2090-0678

Online ISSN

2636-364X

Article File

ASAT_Volume 12_Issue ASAT Conference, 29-31 May 2007_Pages 1-17.pdf

PDF . 263.3kB

Link

https://asat.journals.ekb.eg/article_23976.html

Detail API

https://asat.journals.ekb.eg/service?article_code=23976

Order

57

Type

Original Article

Type Code

737

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

https://asat.journals.ekb.eg/

MainTitle

DESIGN OF THE GUIDANCE, NAVIGATION AND CONTROL SYSTEM OF A LUNAR LANDER

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Article

Created At

22 Jan 2023