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Optical Engineering

Volumn 36, Issue 5, 1997, Pages 1552-1561

Trade-off study and computer simulation for assessing spacecraft pointing accuracy and stability capabilities

(2) Algrain, Marcelo C a,b,c,d,e,f,g,h Powers, Richard M b,i

a International Society for Optics and Photonics (United States)

b UNIVERSITY OF NEBRASKA LINCOLN (United States)

c WRIGHT STATE UNIVERSITY (United States)

d ILLINOIS INSTITUTE OF TECHNOLOGY (United States)

e Recon/Optical Inc (United States)

f Borg Warner Research (United States)

g IEEE (United States)

h AIAA (United States)

i UNIVERSITY OF COLORADO (United States)

Author keywords

Gyros; Kalman filter; Pointing accuracy and stability; Star trackers

Indexed keywords

EID: 0344705548 PISSN: 00913286 EISSN: None Source Type: Journal
DOI: 10.1117/1.601377 Document Type: Article

Times cited : (2)

References (9)

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2
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4
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- Beer, F.¹ Johnston, E.²

5
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- Rotational Kinematics
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7
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- Applications and Additional Topics on Discrete Kalman Filtering
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- Brown, R.¹ Hwang, P.²

8
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9
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- Kalman filtering for spacecraft attitude determination
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- E. Lefferts, F. Markley, and M. Shuster, "Kalman filtering for spacecraft attitude determination," AIAA J. Guid. 5, 417-429 (Sep.-Oct. 1982).
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- Lefferts, E.¹ Markley, F.² Shuster, M.³

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