Improvements in lunar gravity field modeling and orbit determination from SELENE multi-satellite tracking data types
نویسندگان
چکیده
The launch of SELENE, which acquired the first direct tracking data over the farside of the Moon by the use of 4-way Doppler data between a relay satellite and the main satellite, has resulted in a dramatic improvement of the knowledge of the global lunar gravity field[1,2]. In addition to the 4-way Doppler data, same-beam differential VLBI data between the two sub-satellites and two stations on Earth were also collected using the VERA network, and foreign stations in two international campaigns. The strength of differential VLBI data derives from the differencing out of common measurement errors, resulting in a precise measurement. Together with the SELENE 2-way and 4-way tracking data and historical tracking data, the VLBI data were processed into a new lunar gravity field model called SGM100i[3] (Fig. 1). The use of VLBI data allow longer arc lengths for the subsatellites, increasing the sensitivity with respect to the lower degrees of the gravity field model. The resulting model shows a drastically improved performance in orbit determination, especially for edge-on geometries (where the satellite orbits over the deep farside). Correlations with topography also show an increase over the farside.
منابع مشابه
Selene (kaguya) Orbit Determination Results and Lunar Gravity Field Estimation by Using 4-way Doppler Measurements
SELENE (Kaguya) is Japan’s first large lunar explorer aims to obtain the scientific data to investigate the origin and the evolution of the moon and to acquire engineering techniques for the future moon exploration and utilization. The nominal mission phase finished at the end of October 2008, and the extended mission phase started from the beginning of November 2008. In order to perform the ad...
متن کاملDetermination of the best-fitting reference orbit for a LEO satellite using the Lagrange coefficients
Linearization of the nonlinear equations and iterative solution is the most well-known scheme in many engineering problems. For geodetic applications of the LEO satellites, e.g. the Earth’s gravity field recovery, one needs to provide an initial guess of the satellite location or the so-called reference orbit. Numerical integration can be utilized for generating the reference orbit if a satelli...
متن کاملGravity acceleration at the sea surface derived from satellite altimetry data using harmonic splines
Gravity acceleration data have grand pursuit for marine applications. Due to environmental effects, marine gravity observations always hold a high noise level. In this paper, we propose an approach to produce marine gravity data using satellite altimetry, high-resolution geopotential models and harmonic splines. On the one hand, harmonic spline functions have great capability for local gravity ...
متن کاملErs Orbit Determination and Gravity Field Model Tailoring: Recent Developments
In the last ten years significant advances have been made in gravity field modelling, culminating in general-purpose models like JGM-3, TEG-3 and EGM96. Significant defects remain in the quality of the models when applied to orbit determination of some altimeter satellites, leading to large orbit errors, characterised by the geographically-correlated nature of the altimeter crossover height dif...
متن کاملDynamic orbit determination and gravity field model improvement from GPS, DORIS and Laser measurements on TOPEX/POSEIDON satellite
In the framework of the GRIM series of gravity field models, the CNES/GRGS GINS precise orbit determination software has been adapted to dynamic GPS data processing. That is simultaneous processing of all available observables (i.e. GPS, DORIS, Laser) and all available satellite orbits (i.e. GPS, TOPEX/POSEIDON) can now be performed. The TOPEX/POSEIDON (T/P) mission satellite is equipped with a...
متن کامل