2021
DOI: 10.1007/s00190-020-01467-4
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Processing of laser altimeter time-of-flight measurements to geodetic coordinates

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Cited by 10 publications
(24 citation statements)
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References 38 publications
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“…From the brief description of the MOLA PEDR geolocation process [33], we inferred that they have accounted for the motion of the spacecraft during times-of-flight, but have not mentioned anything about pointing aberration or other forms of pointing correction. Thus, we applied the SMM geolocation model with Mars as the observer for the recomputation [21]:…”
Section: Methodsmentioning
confidence: 99%
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“…From the brief description of the MOLA PEDR geolocation process [33], we inferred that they have accounted for the motion of the spacecraft during times-of-flight, but have not mentioned anything about pointing aberration or other forms of pointing correction. Thus, we applied the SMM geolocation model with Mars as the observer for the recomputation [21]:…”
Section: Methodsmentioning
confidence: 99%
“…Given the trajectory and attitude of the spacecraft, pointing alignment of the laser altimeter, and rotational model of the target body, the time-of-flight measurements can be converted to surface coordinates in the body-fixed reference frame of the target body, i.e., the geolocation process. In a previous work, we presented a consistent and systematic formulation of three commonly-used geolocation models with increasing complexity: Static Model (SM), Spacecraft Motion Model (SMM), and Pointing Aberration Model (PAM) [21]. Furthermore, the Special Relativity Model (SRM) is proposed to take care of the special relativity effects, which have been analytically demonstrated to be equivalent to PAM given some assumptions.…”
Section: Introductionmentioning
confidence: 99%
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“…Furthermore, we take into account the pointing aberration induced by special relativity. For the nadir-pointing profiles, this factor can lead to lateral shifts of less than 5 m and radial ones of less than 5 cm, whereas these values can be as high as 10 m and 25 m, respectively, for the intermittently acquired profiles with off-nadir pointing angles up to 35° (Xiao et al, 2021). These off-nadir profiles were acquired by commanding MGS to roll off-nadir >10°to fill the gaps beyond the orbital limits of ∼87°S/N, and have amounted to more than 100 throughout the mission.…”
Section: State Of the Art Reprocessingmentioning
confidence: 99%
“…Furthermore, the intersection angles of profiles forming these non-polar cross-overs can be shallow, which makes them vulnerable to cross-track components of profile lateral shifts due to residual errors. Even limited cross-track displacements are capable of shifting these intersection points dramatically upwards or downwards along the near-parallel profiles, compromising the measured cross-over height differences (Xiao et al, 2021, see also Sec. 6.2).…”
Section: Potential Applicationsmentioning
confidence: 99%