Spacecraft Angular Rate Estimation from Magnetometer Data Only Using an Analytic Predictor
Author:
Affiliation:
1. University of Bologna, 47100 Forli, Italy
2. Technion—Israel Institute of Technology, 32000 Haifa, Israel
3. University of Rome “La Sapienza,”, 00184 Rome, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.10332
Reference23 articles.
1. Kalman Filtering for Spacecraft Attitude Estimation
2. Three-axis attitude determination via Kalman filtering of magnetometer data
3. Satellite Angular Rate Estimation from Vector Measurements
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