Spin-Axis Attitude Determination Program for the Geosynchronous Transfer Orbit Spacecraft

Details Spin-Axis Attitude Determination Program for the Geosynchronous Transfer Orbit Spacecraft Spin-Axis Attitude Determination Program for the Geosynchronous Transfer Orbit Spacecraft

Jun 1993

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1993jass...10....1l&link_type=abstract

Journal of Astronomy and Space Sciences, vol.10, no 1, p.1-16.

Astronomy and Astrophysics

Astronomy

Scientific paper

Three types of spin-axis attitude determination program for the geosynchronous transfer orbit spacecraft are developed. Deterministic closed-form algorithm, batch least-square algorithm and stabilized Kalman filter algorithm are used for implemetation of three programs. EUROSTAR bus model from Birtish Aerospace is used for attitude sensor modelling. Attitude determinations using three programs are performed for the simulated sensor data according to INMARSAT 2-F1 prelaunch mission analysis.

Affiliated with

Also associated with

No associations

Rating

Spin-Axis Attitude Determination Program for the Geosynchronous Transfer Orbit Spacecraft 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 Spin-Axis Attitude Determination Program for the Geosynchronous Transfer Orbit Spacecraft, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Spin-Axis Attitude Determination Program for the Geosynchronous Transfer Orbit Spacecraft will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-1333961