Ballistic Coefficient Estimation for Low Altitude Debris Objects from Two-Line Element Data

Author(s):  
Michael Afful ◽  
Steven Gehly ◽  
Han Cai ◽  
Kefei Zhang
2017 ◽  
Vol 2017 ◽  
pp. 1-13 ◽  
Author(s):  
David J. Gondelach ◽  
Roberto Armellin ◽  
Aleksander A. Lidtke

Spent rocket bodies in geostationary transfer orbit (GTO) pose impact risks to the Earth’s surface when they reenter the Earth’s atmosphere. To mitigate these risks, reentry prediction of GTO rocket bodies is required. In this paper, the reentry prediction of rocket bodies in eccentric orbits based on only Two-Line Element (TLE) data and using only ballistic coefficient (BC) estimation is assessed. The TLEs are preprocessed to filter out outliers and the BC is estimated using only semimajor axis data. The BC estimation and reentry prediction accuracy are analyzed by performing predictions for 101 rocket bodies initially in GTO and comparing with the actual reentry epoch at different times before reentry. Predictions using a single and multiple BC estimates and using state estimation by orbit determination are quantitatively compared with each other for the 101 upper stages.


2012 ◽  
Vol 49 (1) ◽  
pp. 175-184 ◽  
Author(s):  
Arrun Saunders ◽  
Graham G. Swinerd ◽  
Hugh G. Lewis
Keyword(s):  

2012 ◽  
Vol 35 (5) ◽  
pp. 1483-1491 ◽  
Author(s):  
Carolin Früh ◽  
Thomas Schildknecht

Author(s):  
You Geun Oh ◽  
Joohwan Chun ◽  
Kwang Yong Jung ◽  
Nam Moon Kim

IEEE Access ◽  
2019 ◽  
Vol 7 ◽  
pp. 129537-129550 ◽  
Author(s):  
Xue Bai ◽  
Chuan Liao ◽  
Xiao Pan ◽  
Ming Xu

2008 ◽  
Vol 41 (7) ◽  
pp. 1115-1122 ◽  
Author(s):  
Eelco Doornbos ◽  
Heiner Klinkrad ◽  
Pieter Visser

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