مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Persian Verion

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

video

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

sound

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Persian Version

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

View:

971
مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Download:

0
مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Cites:

Information Journal Paper

Title

SATELLITE PASSES SIMULATION AND CALCULATING THE SATELLITE RISE AND SET TIMES FOR THE SITE

Pages

  29-38

Abstract

 One of the most important issues in the productivity of the satellites is the mode timing and the automatic writing of the scenario on-board of the satellite with regard environmental conditions. In order to have the capability to make flight scenarios for missions sent from ground stations or missions that are generated automatically, on board timing forecast along with the time to reach the station or the photo target will be necessary.On board automatic generation of the scenarios will reduce the dependency of the satellite to ground station. Calculation of the SATELLITE RISE AND SET times, without the satellite passes and orbit disturbances simulation, would not be possible.This paper presents formula for the satellite passes simulation, algorithm and time prediction computation modeling using keplerian orbital parameters and reduces the size of the calculation utilizing of semimajor axis of the orbit to be used on the board of satellite.To reduce the volume of calculations, it will be necessary to use numerical methods for finding function minimums or roots. semimajor axis of the orbit will decrease the numerical computation to a great extent using the algorithm presented in this paper.

Cites

  • No record.
  • References

  • No record.
  • Cite

    APA: Copy

    DANESHNIA, EHSAN, NASIRIAN, MEHRZAD, & DEHGHAN, SEYED MOHAMMAD MAHDI. (2013). SATELLITE PASSES SIMULATION AND CALCULATING THE SATELLITE RISE AND SET TIMES FOR THE SITE. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), 5(4 (13)), 29-38. SID. https://sid.ir/paper/150021/en

    Vancouver: Copy

    DANESHNIA EHSAN, NASIRIAN MEHRZAD, DEHGHAN SEYED MOHAMMAD MAHDI. SATELLITE PASSES SIMULATION AND CALCULATING THE SATELLITE RISE AND SET TIMES FOR THE SITE. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST)[Internet]. 2013;5(4 (13)):29-38. Available from: https://sid.ir/paper/150021/en

    IEEE: Copy

    EHSAN DANESHNIA, MEHRZAD NASIRIAN, and SEYED MOHAMMAD MAHDI DEHGHAN, “SATELLITE PASSES SIMULATION AND CALCULATING THE SATELLITE RISE AND SET TIMES FOR THE SITE,” JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), vol. 5, no. 4 (13), pp. 29–38, 2013, [Online]. Available: https://sid.ir/paper/150021/en

    Related Journal Papers

    Related Seminar Papers

  • No record.
  • Related Plans

  • No record.
  • Recommended Workshops






    Move to top
    telegram sharing button
    whatsapp sharing button
    linkedin sharing button
    twitter sharing button
    email sharing button
    email sharing button
    email sharing button
    sharethis sharing button