TY - GEN
T1 - Using a Single Imager and Structured Light for High Resolution and Accurate 3D Mapping of Microscopic Terrain on Mars
AU - Klevang, David Arge
AU - Nielsen, Jonas H.
AU - Henneke, Jesper
AU - Wade, Lawrence A.
AU - Nemere, Peter
AU - Morantz, Chaz
AU - Jorgensen, Peter S.
AU - Tallarida, Nick
AU - Benn, Mathias
AU - Flannery, David
AU - Randazzo, Nicolas
AU - Denver, Troelz
AU - Jorgensen, John L.
AU - Cable, Morgan
AU - Hurowitz, Joel
AU - Allwood, Abigail
N1 - Publisher Copyright:
© 2026 IEEE.
PY - 2026
Y1 - 2026
N2 - The navigational sensor onboard PIXL, the Micro Context Camera, is equipped with active LED multispectral floodlight and laser structured light capabilities. The first ensures a homogeneous lighted scene, to capture the optical context of the surface. The structured light consists of 2 illumination sources, each with their individual dot pattern projected onto the surface: One designed to keep optimal distance along the ∼ 120 μ m XRF pencil beam, during PIXL's XRF scan, and one designed for broad coverage enabling safe assessment of the terrain. By virtue of triangulation, including thermal calibration, the distance to the terrain is measured to accuracies of ∼ 50 microns. While the structured light offers very accurate absolute range measurements, the projected dot pattern is sparse, leaving much terrain area uncovered. The aim here is to resolve a high terrain resolution, making use of the accurate range measurements using the structured light. Often a terrain is resolved without the scaling dimension, and only produces a disparity map. To resolve the scale factor, one could rely on the actual motion between two observations, i.e. the baseline. However, due to significant positional drift due to the thermal environment on Mars, the usage of the structured light provides the scale factor. Instead, we merge the best of both worlds, applying a highly accurate range measurement to a high-resolution disparity map. This approach makes use of the motion capabilities of PIXL, using the hexapod actuator, or the robotic arm of the rover, but is not dependent on any motion metrology knowledge. Furthermore, this approach can be utilized on any single imager system with structured light and actuator capabilities.
AB - The navigational sensor onboard PIXL, the Micro Context Camera, is equipped with active LED multispectral floodlight and laser structured light capabilities. The first ensures a homogeneous lighted scene, to capture the optical context of the surface. The structured light consists of 2 illumination sources, each with their individual dot pattern projected onto the surface: One designed to keep optimal distance along the ∼ 120 μ m XRF pencil beam, during PIXL's XRF scan, and one designed for broad coverage enabling safe assessment of the terrain. By virtue of triangulation, including thermal calibration, the distance to the terrain is measured to accuracies of ∼ 50 microns. While the structured light offers very accurate absolute range measurements, the projected dot pattern is sparse, leaving much terrain area uncovered. The aim here is to resolve a high terrain resolution, making use of the accurate range measurements using the structured light. Often a terrain is resolved without the scaling dimension, and only produces a disparity map. To resolve the scale factor, one could rely on the actual motion between two observations, i.e. the baseline. However, due to significant positional drift due to the thermal environment on Mars, the usage of the structured light provides the scale factor. Instead, we merge the best of both worlds, applying a highly accurate range measurement to a high-resolution disparity map. This approach makes use of the motion capabilities of PIXL, using the hexapod actuator, or the robotic arm of the rover, but is not dependent on any motion metrology knowledge. Furthermore, this approach can be utilized on any single imager system with structured light and actuator capabilities.
UR - https://www.scopus.com/pages/publications/105041376897
U2 - 10.1109/AERO66936.2026.11519995
DO - 10.1109/AERO66936.2026.11519995
M3 - Conference contribution
AN - SCOPUS:105041376897
T3 - IEEE Aerospace Conference Proceedings
BT - 2026 IEEE Aerospace Conference, AERO 2026
PB - IEEE Computer Society
T2 - 2026 IEEE Aerospace Conference, AERO 2026
Y2 - 7 March 2026 through 14 March 2026
ER -