Computer Science – Performance
Scientific paper
Aug 1984
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1984adans..54.1265w&link_type=abstract
IN: Astrodynamics 1983; Proceedings of the Conference, Lake Placid, NY, August 22-25, 1983. Part 2 (A84-30526 13-13). San Diego,
Computer Science
Performance
Geosynchronous Orbits, Kalman Filters, Orbit Calculation, Parameter Identification, Synchronous Satellites, Trajectory Analysis, Error Analysis, Orbit Perturbation, Orbital Elements, Run Time (Computers), Statistical Analysis
Scientific paper
It is noted that the ANIK A1 study made it possible to evaluate the performance for synchronous satellites of the semianalytical orbit determination system. The development and current operation of semianalytical satellite theory and the associated semianalytical sequential estimator are summarized, and the test procedures and results are presented. While demonstrating the flexibility of the Goddard trajectory determination system (GTDS) as a research tool, the ANIK A1 study provided an opportunity to evaluate all four GTDS-based estimators in a real data test case. It is pointed out that the Cowell and semianalytical differential corrections batch estimators produced epoch solve-for states that resulted in quite similar observation residual statistics when used in special perturbations and semianalytical propagators, respectively.
No associations
LandOfFree
Application of the extended semianalytical Kalman filter to synchronous orbits 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 Application of the extended semianalytical Kalman filter to synchronous orbits, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Application of the extended semianalytical Kalman filter to synchronous orbits will most certainly appreciate the feedback.
Profile ID: LFWR-SCP-O-1673812