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Sensitivity threshold development

  1. Jun 23, 2015 #1
    I am trying to develop a sensitivity analysis tool and I would appreciate it if anyone had any information on how does the error in the semimajor axis and/or other orbital elements of the orbit of a LEO satellite influence the error in pitch, yaw and roll angles?
  2. jcsd
  3. Jun 28, 2015 #2
    Thanks for the post! This is an automated courtesy bump. Sorry you aren't generating responses at the moment. Do you have any further information, come to any new conclusions or is it possible to reword the post?
  4. Jun 29, 2015 #3
    The question is how the errors in measuring or predicting orbital elements for a LEO, sunsynchronous satellite, affect Earth scene pointing.
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