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Averaged spin state catalog framework for uncontrolled space objects
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DOI：10.1016/j.asr.2026.02.040.png)
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Abstract
En 中文
• Develop space object spin state catalog framework using averaged attitude dynamics. • Estimate inertial spin rate, axis, and external torque coefficients using light curve spin rates. • Converge on simulated truth in 1 year with sparse spin rates and no prior object knowledge. • For real Telstar 401 measurements, obtain solution consistent with independent radar data.
Keywords:
Attitude dynamics
Estimation
Satellite characterization
Light curves
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