Physics – Space Physics
Scientific paper
2010-02-11
Adv. Space Res., 47, 7, 1107-1115 (2011)
Physics
Space Physics
Submitted to Advances in Space Research. 13 pages, 4 figures
Scientific paper
10.1016/j.asr.2010.10.017
The density of orbital space debris constitutes an increasing environmental challenge. There are three ways to alleviate the problem: debris mitigation, debris removal and collision avoidance. This paper addresses collision avoidance, by describing a method that contributes to achieving a requisite increase in orbit prediction accuracy. Batch least-squares differential correction is applied to the publicly available two-line element (TLE) catalog of space objects. Using a high-precision numerical propagator, we fit an orbit to state vectors derived from successive TLEs. We then propagate the fitted orbit further forward in time. These predictions are compared to precision ephemeris data derived from the International Laser Ranging Service (ILRS) for several satellites, including objects in the congested sun-synchronous orbital region. The method leads to a predicted range error that increases at a typical rate of 100 meters per day, approximately a 10-fold improvement over TLE's propagated with their associated analytic propagator (SGP4). Corresponding improvements for debris trajectories could potentially provide initial conjunction analysis sufficiently accurate for an operationally viable collision avoidance system. We discuss additional optimization and the computational requirements for applying all-on-all conjunction analysis to the whole TLE catalog, present and near future. Finally, we outline a scheme for debris-debris collision avoidance that may become practicable given these developments.
Levit Creon
Marshall William
No associations
LandOfFree
Improved orbit predictions using two-line elements does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.
If you have personal experience with Improved orbit predictions using two-line elements, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Improved orbit predictions using two-line elements will most certainly appreciate the feedback.
Profile ID: LFWR-SCP-O-67925