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Sensor Data Fusion For Hazard Mapping And Piloting

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HAL Id: hal-01396797

https://hal.inria.fr/hal-01396797

Submitted on 16 Nov 2016

HAL is a multi-disciplinary open access archive for the deposit and dissemination of sci- entific research documents, whether they are pub- lished or not. The documents may come from teaching and research institutions in France or abroad, or from public or private research centers.

L’archive ouverte pluridisciplinaire HAL, est destinée au dépôt et à la diffusion de documents scientifiques de niveau recherche, publiés ou non, émanant des établissements d’enseignement et de recherche français ou étrangers, des laboratoires publics ou privés.

Sensor Data Fusion For Hazard Mapping And Piloting

Keyvan Kanani, Roland Brochard, Florent Hennart, Alexandre Pollini, Peter Sturm, Olivier Dubois-Matra, Sanjay Vijendran

To cite this version:

Keyvan Kanani, Roland Brochard, Florent Hennart, Alexandre Pollini, Peter Sturm, et al.. Sensor Data Fusion For Hazard Mapping And Piloting. 13th International Planetary Probe Workshop, Jun 2016, Laurel, United States. �hal-01396797�

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The HDA system is assessed within a complete GNC simulator, with image simulation and processing (point tracking and LiDAR altimetry) in the loop. It includes realistic sensor data simulation, and considers real Mars and asteroid terrains, extracted from NASA’s PDS database.

SENSOR DATA FUSION FOR HAZARD AVOIDANCE

K. Kanani1, R. Brochard1, F. Hennart1, A. Pollini2, P. Sturm3, O. Dubois-Matra4, S. Vijendran4.

1Airbus Defence & Space, 2CSEM, 3INRIA Grenoble Rhône-Alpes, 4ESA-ESTEC.

Autonomous landing on Mars, Moon or asteroids may require an autonomous Hazard Detection and Avoidance (HDA) system. Past studies on HDA or actual missions (such as Chang’E 3) dealt with the use of camera or LiDARs separately to detect dangerous slopes, boulders and shadowed areas. The present work, performed in the frame of an ESA Technology Research Program, proposes to use jointly a camera and a LiDAR to take advantage of each while mitigating their drawbacks, consequently improving the HDA performances. Various algorithmic solutions and sensor configurations are proposed and tested in the Mars and asteroid landing cases.

Sensor configuration

Simulated camera image and LIDAR FoV (orange: receiver, red: laser)

Hazard mapping

GNC simulator

LIDAR noise simulation

The selected LiDAR is a last-generation TOF camera built by CSEM, using a laser source modulated in amplitude. The chosen camera is based on heritage from ESA and NASA studies.

0 80

40 -5

5 0

LiDAR Denoising Ground truth

3D reconstruction with nav error 3D reconstruction without nav error

Safe slope classification Hazard map

HDA solution is conservative:

Very low false positive rate

(no unsafe site detected as safe in our tests)

Low detection rate

(only a few available safe sites are detected, but always one!)

Our HDA solution starts with a temporal and spatial denoising of the LiDAR signal. A 3D reconstruction is then performed using LiDAR and camera measurements. A classification step, based on machine learning, is then applied to improve slope map. The slope map is finally combined with shadow and roughness maps, using a fuzzy logic technique to select a safe landing site.

GNC performances at touchdown:

Vertical velocity < 0.6m/s

Horizontal velocity < 0.4m/s

Attitude rate < 10mdeg/s

Z-axis angle < 0.1deg/s

LS position < 1m

1st HA

2d HA Mars landing

trajectory Hazard

maps

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