An Improved Angular Rate Estimation Using Only Star Sensor Measurement
Author:
Affiliation:
1. Satellite and Space Exploration Systems Engineering and Architecture Research and Development Division, Korea Aerospace Research, Daejeon, South Korea
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Link
http://xplorestaging.ieee.org/ielx7/7361/10530892/10494215.pdf?arnumber=10494215
Reference32 articles.
1. Spacecraft angular rate estimation algorithms for star tracker-based attitude determination;Singla;Adv. Astron. Sci.,2003
2. Hubble space telescope reduced-gyro control law design, implementation, and on-orbit performance;Clapp
3. Robust attitude determination without rate gyros;Mook,1993
4. Gyro-free attitude and rate estimation for a small satellite using SVD and EKF
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