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 - Jørgensen, John L.
AU - Cable, Morgan
AU - Hurowitz, Joel
AU - Allwood, Abigail
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 ∼120μm
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 ∼120μm
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.
U2 - 10.1109/AERO66936.2026.11519995
DO - 10.1109/AERO66936.2026.11519995
M3 - Article in proceedings
T3 - IEEE Aerospace Conference Proceedings
SP - 1
EP - 9
BT - 2026 IEEE Aerospace Conference
PB - IEEE
T2 - 2026 IEEE Aerospace Conference
Y2 - 7 March 2026 through 14 March 2026
ER -