LEADER 03559nam  22006614a 450 
001 9910146061503321
005 20170815114456.0
010   $a1-280-25334-7
010   $a9786610253340
010   $a0-470-35723-1
010   $a0-471-72617-6
010   $a0-471-72847-0
035   $a(CKB)1000000000019065
035   $a(EBL)226452
035   $a(OCoLC)181838508
035   $a(SSID)ssj0000157307
035   $a(PQKBManifestationID)11155881
035   $a(PQKBTitleCode)TC0000157307
035   $a(PQKBWorkID)10130455
035   $a(PQKB)10166663
035   $a(MiAaPQ)EBC226452
035   $a(EXLCZ)991000000000019065
100   $a20021023d2003      uy             0
101 0 $aeng
135   $aur|n|---|||||
181   $ctxt
182   $cc
183   $acr
200 10$aFormulation for observed and computed values of Deep Space Network data types for navigation$b[electronic resource] /$fTheodore D. Moyer
210   $aHoboken, N.J. $cWiley-Interscience$dc2003
215   $a1 online resource (573 p.)
225 1 $aDeep-space communications and navigation series
300   $aDescription based upon print version of record.
311   $a0-471-44535-5 
320   $aIncludes bibliographical references (p. 539-545) and index.
327   $aFormulation for Observed and Computed Values of Deep Space Network Data Types for Navigation; Contents; Foreword; Preface; Acknowledgments; 1 Introduction; 2 Time Scales and Time Differences; 3 Planetary Ephemeris, Small-Body Ephemeris, and Satellite Ephemerides; 4 Spacecraft Ephemeris and Partials File; 5 Geocentric Space-Fixed Position, Velocity, and Acceleration Vectors of Tracking Station; 6 Space-Fixed Position, Velocity, and Acceleration Vectors of a Landed Spacecraft Relative to Center of Mass of Planet, Plan; 7 Algorithms for Computing ET-TAI; 8 Light-Time Solution; 9 Angles
327   $a10 Media and Antenna Corrections11 Calculation of Precision Light Times and Quasar Delays; 12 Partial Derivatives of Precision Light Times and Quasar Delays; 13 Observables; 14 References; 15 Acronyms; Index
330   $aA valuable reference for students and professionals in the field of deep space navigationDrawing on fundamental principles and practices developed during decades of deep space exploration at the California Institute of Technology's Jet Propulsion Laboratory (JPL), this book documents the formation of program Regres of JPL's Orbit Determination Program (ODP). Program Regres calculates the computed values of observed quantities (e.g., Doppler and range observables) obtained at the tracking stations of the Deep Space Network, and also calculates media corrections for the computed values o
410  0$aDeep-space communications and navigation series.
606   $aSpace vehicles$xTracking$xData processing
606   $aNavigation (Astronautics)$xMathematics
606   $aDeep Space Network
606   $aSpace trajectories$xData processing
608   $aElectronic books.
615  0$aSpace vehicles$xTracking$xData processing.
615  0$aNavigation (Astronautics)$xMathematics.
615  0$aDeep Space Network.
615  0$aSpace trajectories$xData processing.
676   $a629.47/43/0285
676   $a629.47430285
700   $aMoyer$b Theodore D$0944432
801  0$bMiAaPQ
801  1$bMiAaPQ
801  2$bMiAaPQ
906   $aBOOK
912   $a9910146061503321
996   $aFormulation for observed and computed values of Deep Space Network data types for navigation$92131942
997   $aUNINA