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Crater Navigation System for Autonomous Precision Landing on the Moon

Maass, Bolko and Woicke, Svenja and Oliveira, Willem and Razgus, Bronislovas and Krüger, Hans (2020) Crater Navigation System for Autonomous Precision Landing on the Moon. Journal of Guidance, Control, and Dynamics. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.G004850. ISSN 0731-5090.

Full text not available from this repository.

Official URL: https://arc.aiaa.org/doi/10.2514/1.G004850

Abstract

Interest in autonomous planetary precision landing missions has been increasing in the scientific and engineering community, and is likely to continue to do so for the foreseeable future. As an enabling technology in the context of lunar landing, DLR, German Aerospace Center has been developing a terrain absolute navigation system that matches craters detected in image data to globally available lunar crater maps. The proposed Crater Navigation (CNav) system is adaptive, comprising three different crater matching methods that are specifically tailored to different navigation conditions encountered during the vehicle descent, so that it may be used as a stand-alone navigation sensor that can be closely integrated with a lander guidance, navigation, and control system to enable reliable absolute navigation throughout the entire descent phase of a mission. As robustness is a vital aspect to mission success, the CNav system includes verification mechanisms that ensure high dependability of the resulting navigation solution. This robustness is verified separately for all of the three different matching techniques presented in this paper. Closed-loop performance of the matchers is demonstrated as well, both for simulated image data sets, as for navigation camera images acquired during the Chinese Chang’e-3 landing mission. Successful uninterrupted estimation of the entire Chang’e-3 kinematic vehicle state during the powered descent until a final altitude of 350 m above ground, with neither known camera calibration nor inertial measurement unit data available, showcases the potential of the CNav system.

Item URL in elib:https://elib.dlr.de/134839/
Document Type:Article
Title:Crater Navigation System for Autonomous Precision Landing on the Moon
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Maass, BolkoBolko.Maass (at) dlr.deUNSPECIFIED
Woicke, SvenjaSvenja.Woicke (at) dlr.dehttps://orcid.org/0000-0002-0864-9977
Oliveira, WillemWillem.MagalhaesOliveira (at) dlr.deUNSPECIFIED
Razgus, BronislovasBronislovas.Razgus (at) dlr.deUNSPECIFIED
Krüger, HansHans.Krueger (at) dlr.deUNSPECIFIED
Date:20 April 2020
Journal or Publication Title:Journal of Guidance, Control, and Dynamics
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
DOI :10.2514/1.G004850
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
ISSN:0731-5090
Status:Published
Keywords:terrain absolute navigation, crater navigation, lunar landing, moon, navigation, GNC, landing GNC
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space System Technology
DLR - Research area:Raumfahrt
DLR - Program:R SY - Space System Technology
DLR - Research theme (Project):R - Projekt ATON (old)
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Navigation and Control Systems
Deposited By: Woicke, Dr Svenja
Deposited On:08 May 2020 11:32
Last Modified:08 May 2020 11:32

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