Results 301 to 310 of about 3,161,815 (352)

Shooting Scheme for Perturbations in Optimised Solution of the Orbital Boundary Value Problem. [PDF]

Aerotec Missili Spaz
Vananti A, Mann HK, Schildknecht T.
europepmc   +1 more source

Adjusted Optical Properties for Galileo, BDS and QZSS Satellites from Precise Orbit Determination

, 2018
Bingbing Duan, Urs Hugentobler, Inga Selmke, Max Hofacker   +3 more
openalex   +1 more source

Precise detection of tiny birefringence with accuracy reaching 10^-11 level. [PDF]

Nat Commun
Zhang X, Hu Y, Zhou S, Zeng Z, Liu G, Lin H, Li Z, Chen Z, Fu S.   +8 more
europepmc   +1 more source

Extended Kalman Filtering of Satellite Doppler Tracking Data and IT¡¯S Application to Orbit Determination Problems

, 1995
Dong‐Kyu Kim, Kyu-Hong Choi
openalex   +1 more source

Enhancing reliability and efficiency of flight dynamics systems for planetary exploration through KPLO ground operation experience. [PDF]

Sci Rep
Song YJ, Bang J, Bae J, Hong S, Kim D, Lee D.   +5 more
europepmc   +1 more source

Methods for the Orbit Determination of a Tethered Satellite System by a Single Ground Station

, 2003
Yuji Sakamoto, Tetsuo Yasaka
openalex   +1 more source

THEORY OF ORBIT DETERMINATION - PART II, ESTIMATION FORMULAS

, 1963
J. D. Anderson
openalex   +1 more source

New Orbit Determination and Clock synchronisation modules for EGNOS

, 2016
R. Lembachar, Thierry Authié, Sébastien Trilles, F. Mercier   +3 more
openalex   +1 more source

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Noncooperative LEO Satellite Orbit Determination Based on Single Pass Doppler Measurements

IEEE Transactions on Aerospace and Electronic Systems, 2023
Precise orbit information is the premise of the wide application of low-Earth-orbit (LEO) satellites. Traditional orbit determination (OD) methods have disadvantages of poor reliability, high hardware cost, and long OD time.
Ruofan Deng, H. Qin, Haotian Li, Danyao Wang, Hongli Lv   +4 more
semanticscholar   +1 more source

Assessing Machine Learning for LEO Satellite Orbit Determination in Simultaneous Tracking and Navigation

IEEE Aerospace Conference, 2021
Machine learning for orbit determination of low Earth orbit (LEO) satellites in a simultaneous tracking and navigation (STAN) framework is assessed. STAN is a navigation paradigm that aims to exploit LEO satellites, which are not intended for navigation ...
Trier Mortlock, Z. Kassas
semanticscholar   +1 more source