AIAA-2006-6597 Vector Observations-Based Gyroless Spacecraft Attitude/Angular Rate Estimation Using Particle Filtering
AIAA guidance, navigation and control conference ; 2006 ; Keystone, Colo
2006-01-01
17 pages
Paper numbers 2006-6037 to 6807 with gaps held
Aufsatz (Konferenz)
Englisch
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