1998
DOI: 10.1007/s001900050158
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Improvement of the empirical thermospheric model DTM: DTM94 - a comparative review of various temporal variations and prospects in space geodesy applications

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Cited by 154 publications
(68 citation statements)
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“…The background GPS solar radiation pressure (SRP) model, GSPM13 , is based on an empirical approach described by Bar-Sever and Kuang [2004], in which the force is represented as a truncated Fourier expansion about the Earth-Satellite-Sun angle. In order to support greater accumulation (and observability) of SRP errors, long integrations of 5 to 10 days are used.…”
Section: Appendix A: On the Independence Of The Dynamical Modelsmentioning
confidence: 99%
“…The background GPS solar radiation pressure (SRP) model, GSPM13 , is based on an empirical approach described by Bar-Sever and Kuang [2004], in which the force is represented as a truncated Fourier expansion about the Earth-Satellite-Sun angle. In order to support greater accumulation (and observability) of SRP errors, long integrations of 5 to 10 days are used.…”
Section: Appendix A: On the Independence Of The Dynamical Modelsmentioning
confidence: 99%
“…These orbit restitutions need precise acceleration models, as DORIS satellites orbit at an altitude around 800 km, where the drag effects cannot be neglected due to the important cross-sectional surface of the platforms. The mathematical model of the orbit trajectory uses, for drag estimation, the DTM94 empirical neutral model (Barlier et al, 1978;Berger et al, 1998). It directly depends on physical parameters, and in particular, the F10.7 solar flux and the Kp geomagnetic indices.…”
Section: Satellite Dragmentioning
confidence: 99%
“…It is based on temperature measurements by the OGO-6 satellite and density data from drag observations. The DTM-94 version (Berger et al, 1998) include data from the microaccelerometer CACTUS (1975CACTUS ( -1979 and from the Dynamic Explorer 2 satellite (1981)(1982)(1983)). This version is actually used for various applications: trajectory computation for satellites such as SPOT or TOPEX/POSEIDON and developments of gravity models.…”
Section: Thermospheric Modelsmentioning
confidence: 99%