Formulation for Observed and Computed Values of Deep Space Network Data Types for Navigation

By T. D. Moyer. 2003

454 citations recorded by the source corpus.

View Paper: https://www.semanticscholar.org/paper/0036b4ae0eb8478f5470da17149b9b52c43e5608

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In Aerospace Engineering

Citations in the corpus

Interior composition, structure and dynamics of the Galilean satellites (2004, methodology): “These coefficients, along with other parameters in the fitting model, are determined from the Galileo radio Doppler data by weighted least squares (Tapley 1973, Anderson 1974, Lawson and Hanson 1974, Moyer 2000).”
Mars high resolution gravity fields from MRO, Mars seasonal gravity, and other dynamical parameters (2011, methodology): “In fitting the Mars range data to the planetary ephemerides, the positions of the planets and Moon were numerically integrated using the Einstein–Infeld–Hoffman equations of motion (Einstein et al., 1938; Moyer, 2000).”
INPOP08, a 4-D planetary ephemeris: from asteroid and time-scale computations to ESA Mars Express and Venus Express contributions (2009, methodology): “The upper triangles represent masses deduced from radar observations as described by Michalak (2000).”
Study of the anomalous acceleration of Pioneer 10 and 11 (2001, methodology): “For each body i (a planet or spacecraft anywhere in the solar system), the point-mass acceleration is written as [39, 40, 46, 51, 52]”
The JPL lunar gravity field to spherical harmonic degree 660 from the GRAIL Primary Mission (2013, methodology): “[33] The GRAIL spacecraft observations were processed using the JPL software MIRAGE; which is a specialized high precision version of the JPL Orbit Determination Program [Moyer, 1971, 2003] developed for the TOPEX mission.”
The Gravity Field of the Saturnian System from Satellite Observations and Spacecraft Tracking Data (2006, methodology): “g Derived from the precession rate of Nicholson et al. (1999). GRAVITY FIELD OF SATURNIAN SYSTEM 2523 No.”
Orbit and bulk density of the OSIRIS-REx target Asteroid (101955) Bennu (2014, methodology): “lativity We used a full relativistic force model including the contribution of the Sun, the planets, and the Moon. More specically, we used the Einstein-Infeld-Homan (EIH) approximation (Will 1993; Moyer 2003; Soel et al. 2003). Table 5 shows the variations in da=dtand 2135 associated with dierent ”
Near Earth Asteroids with measurable Yarkovsky effect (2012, methodology): “Namely, we used the Einstein-InfeldHoffman (EIH) approximation as described in Moyer (2003) or Will (1993).”
Improved methods for observing Earth's time variable mass distribution with GRACE using spherical cap mascons (2015, methodology): “The partial derivatives of the gravitational acceleration with respect to the spacecraft state and model parameters have been derived [Sunseri, 2010] and implemented in the Orbit Determination Program (ODP) [Moyer, 1971, 2000] of the Jet Propulsion Laboratory.”
New constraints on Saturn’s interior from Cassini astrometric data (2015, background): “Peters (1981) and Moyer (2000) describe the orbital models for the satellites and spacecraft, respectively.”
The JPL Planetary and Lunar Ephemerides DE440 and DE441 (2021, methodology): “The directions of the PAs are taken from analyses of the Gravity Recovery and Interior Laboratory (GRAIL) data (Konopliv et al. 2013; Lemoine et al. 2013).”
Precession of Mercury’s Perihelion from Ranging to the MESSENGER Spacecraft (2017, methodology): “This section shows how we actually estimate these fundamental parameters through a dynamical estimation process, i.e., we numerically integrate the PPN governing equations of motion with the LT effect included (Moyer 2000; Folkner et al. 2014).”