Determination of intrack orbital position from earth and sun sensor data

Details Determination of intrack orbital position from earth and sun sensor data Determination of intrack orbital position from earth and sun sensor data

Aug 1975

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1975fmet.symp..213s&link_type=abstract

In NASA. Goddard Space Flight Center Flight Mech./Estimation Theory Symp. p 213-222 (SEE N76-10167 01-12)

Other

Data Processing, Ephemeris Time, Orbital Elements, Orbital Position Estimation, Celestial Reference Systems, Earth Surface, Error Correcting Devices, Orbit Calculation, Orbital Mechanics

Scientific paper

By intrack orbital error is meant a constant time adjustment that is applied to a set of ephemeris data which is otherwise correct. The ephemeris data may be in the form of an orbit tape or in the form of orbital elements with an associated orbit generator. The time adjustment is simply added to the time before the ephemeris routine is accessed. It is implicit here that the time adjustment is a constant throughout the pass of data that are considered, where the pass of data is typically a fraction of one orbit.

Affiliated with

Also associated with

No associations

Rating

Determination of intrack orbital position from earth and sun sensor data does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.

If you have personal experience with Determination of intrack orbital position from earth and sun sensor data, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Determination of intrack orbital position from earth and sun sensor data will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-1537949