Sixth US/Russian Space Surveillance Workshop: August 22-26, 2005, ProceedingsP. Kenneth Seidelmann, Viktor Kuzʹmich Abalakin Central Astronomical Observatory at Pulkovo, Russian Academy of Sciences, 2005 - 319 Seiten |
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Seite 115
... calculations by formula ( 3 ) . As an example , the atmospheric density corrections to the NRLMSIS - 00 model , calculated for 2003 , are given in Fig . 4 for altitudes of 200 , 300 , 400 , 500 and 600 km . From the presented plots it ...
... calculations by formula ( 3 ) . As an example , the atmospheric density corrections to the NRLMSIS - 00 model , calculated for 2003 , are given in Fig . 4 for altitudes of 200 , 300 , 400 , 500 and 600 km . From the presented plots it ...
Seite 120
... calculated for spherical SOs [ 11 ] . Table 4 summarizes the results of the estimations of true ballistic coefficient values that we have obtained for all 16 selected SOs . The first column gives the NORAD catalog numbers for space ...
... calculated for spherical SOs [ 11 ] . Table 4 summarizes the results of the estimations of true ballistic coefficient values that we have obtained for all 16 selected SOs . The first column gives the NORAD catalog numbers for space ...
Seite 196
... calculated for 69 points with the step of 2 minutes , taking into account the secular perturbations only . In Table 1 in the first line the improved values of the orbit elements are given . In the second line the elements of the ...
... calculated for 69 points with the step of 2 minutes , taking into account the secular perturbations only . In Table 1 in the first line the improved values of the orbit elements are given . In the second line the elements of the ...
Inhalt
FOREWORD | 7 |
EVOLVING SPACE SURVEILLANCE CAPABILITIES MATHEMATICAL | 22 |
Orbital Debris | 37 |
Urheberrecht | |
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Häufige Begriffe und Wortgruppen
accuracy algorithm altitude analysis ARIMA Astrodynamics atmospheric model autoregression average b₁ and b₂ b₂ time series ballistic coefficient calculated camera candidate user catalogue computed correlation covariance COWPOKE density model density variations detection difference drag coefficient equations errors estimates explosion extreme user Figure forecasting fragments GEO objects GEO region GEODSS geomagnetic geostationary interval Jacchia Kalman filter Laplace plane latitude longitude magnitude maximum measurements method microradians motion nonlinear filters NRLMSIS-00 model observations Observatory obtained operations optical orbit determination orbital elements particle filter performance parameter perigee perturbations plotted prediction Pulkovo radar re-entry requirements right ascension Russia SATA sensor semiannual variation SGP4 sigma particle Sixth US-Russian Space solar activity solar cycle solar minimum Space Debris space objects Space Surveillance Workshop space weather spacecraft spheres Starshine statistical strategy sunspot Table telescope thermospheric track US-Russian Space Surveillance utility functions vector velocity weights