Analytic steady-state accuracy solutions for two common spacecraft attitude estimators

Journal of Guidance, Control, and Dynamics

Volumn 1, Issue 4, 1978, Pages 282-284

  Farrenkopf, R L ^a  

^a TR WDefense and Space Systems Group ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 85003406366     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.55779     Document Type: Article

References (2)

1. Farrenkopf, R.L., “Generalized Results for Precision Attitude Reference Systems Using Gyros,” AIAA Paper 74-903, Anaheim, Calif., Aug. 1974.
2. Sorenson, H.W., “Kalman Filtering Techniques,” Advances in Control Systems, Vol. 3, Academic Press, New York, 1966, pp. 219-292.