Design and simulation of a three-axis stabilized satellite and Kalman filter rate estimator
Approved for public release; distribution is unlimited === Design requirements for a small satellite (NPSAT-1) Attitude Determination and Control Subsystem (ADCS) is a three-axis stabilized spacecraft which requires a control attitude of +/- 1.0 degrees and knowledge attitude of +/- 0.1 degree. Seve...
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Others |
| Published: |
Monterey, California. Naval Postgraduate School
2012
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/10945/888 |