Record ID | ia:satellitesimulat00shud |
Source | Internet Archive |
Download MARC XML | https://archive.org/download/satellitesimulat00shud/satellitesimulat00shud_marc.xml |
Download MARC binary | https://www.archive.org/download/satellitesimulat00shud/satellitesimulat00shud_meta.mrc |
LEADER: 01914nam 2200289 a 45 0
001 a198388
008 980608s1989 caua b f000|0 eng d
040 $aCMontNP$cCMontNP
086 0 $aD 208.14/2:NPS-55-89-10
100 1 $aShudde, Rex H.
245 12 $aA satellite simulation program /$cRex H. Shudde.
260 $aMonterey, Calif. :$bNaval Postgraduate School ;$aSpringfield, Va. :$bAvailable from National Technical Information Service,$c[1989]
300 $aii, 51 p. :$bill. ;$c28 cm.
500 $aTitle from cover.
500 $a"NPS-55-89-10."
500 $a"September 1989."
500 $aAD A218 079.
504 $aIncludes bibliographical references (p. 49).
520 $aThis report presents a satellite simulation written for the IBM PC and clones in Microsoft QuickBASIC 4.5. The program can either generate an ephemeris of satellite ground-track position and location with respect to a fixed ground station, or determine the position and time the satellite is above the horizon of a specified ground station. Provision is made for the program to handle multiple satellites and multiple ground stations. Input is either by way of the computer keyboard or by separate files for satellites and ground stations. Output is written both on the screen and to an ASCII output file which can be accessed by a data based management program. Keywords: Satellite; Satellite simulation; Satellite vulnerability; Satellite tracking; Satellite orbit; Satellite culmination; Ground track. (JHD)
592 $aaq/aq cc:9116 06/08/98
650 4 $aEPHEMERIDES.
650 4 $aSPACECRAFT TRAJECTORIES.
650 4 $aEARTH ORBITS.
710 2 $aNaval Postgraduate School (U.S.).$bDept. of Operations Research.
740 01 $aNPS-55-89-10.
926 $aNPS-LIB$bDIGIPROJ$cD 208.14/2:NPS-55-89-10$dBOOK$eNEVER$f1
926 $aNPS-LIB$bFEDDOCS$cD 208.14/2:NPS-55-89-10$dBOOK$f2