Analytic Steady-State Accuracy Solutions for Two Common Spacecraft Attitude Estimators
- 1 July 1978
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 1 (4), 282-284
- https://doi.org/10.2514/3.55779
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Satellite attitude acquisition by momentum transferAIAA Journal, 1976
- Perturbation Solution for the Flat Spin Recovery of a Dual-§pin SpacecraftAIAA Journal, 1976
- Generalized results for precision attitude reference systems using gyrosPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974