Steady-State Accuracy Solutions of More Spacecraft Attitude Estimators
- 14 June 2011
- conference paper
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Survey of Nonlinear Attitude Estimation MethodsJournal of Guidance, Control, and Dynamics, 2007
- Optimal Estimation of Dynamic SystemsPublished by Informa UK Limited ,2004
- Kalman Filtering for Spacecraft System Alignment CalibrationJournal of Guidance, Control, and Dynamics, 2001
- Analytic Steady-State Accuracy of a Spacecraft Attitude EstimatorJournal of Guidance, Control, and Dynamics, 2000
- 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