Estimation of spacecraft attitude in the presence of unmodeled disturbance torques
A general approach is presented for the estimation of spacecraft attitude from rate gyroscope measurements of angular velocity and indirect inertial orientation measurements obtained from a pair of star sensors. The estimation algorithm is developed in such a way that the measured minus estimated an...
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Others |
| Language: | en_US |
| Published: |
Virginia Polytechnic Institute and State University
2019
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/10919/87265 |