Analytic Steady-State Accuracy of a Spacecraft Attitude Estimator
- 1 November 2000
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 23 (6) , 1065-1067
- https://doi.org/10.2514/2.4648
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Kalman Filtering for Spacecraft Attitude EstimationJournal of Guidance, Control, and Dynamics, 1982
- Analytic Steady-State Accuracy Solutions for Two Common Spacecraft Attitude EstimatorsJournal of Guidance, Control, and Dynamics, 1978
- Optimum mixing of gyroscope and star tracker data.Journal of Spacecraft and Rockets, 1968
- A New Approach to Linear Filtering and Prediction ProblemsJournal of Basic Engineering, 1960