AIAA-2003-5393 Prediction of Re-Entry of Space Debris Objects: Constant Gain Kalman Filter Approach
Conference, Atmospheric flight mechanics ; 2003 ; Austin, TX
2003-01-01
11 pages
Contains paper nos AIAA-2003-5300 to AIAA-2003-5707 with gaps
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
A constant gain Kalman filter approach for the prediction of re-entry of risk objects
Online Contents | 2007
|AIAA-2003-5392 Entry Vehicle and Jettisoned Debris Recontact Analysis
British Library Conference Proceedings | 2003
|