EngineeringMathematics

Three-axis attitude determination from vector observations

M. Shuster, S. Oh

1981.2.1JOURNAL OF GUIDANCE CONTROL AND DYNAMICS

DOI: 10.2514/3.19717

tlooto Summary

Two computationally efficient algorithms are presented for determining three-axis attitude from two or more vector observations that are useful to the mission analyst or spacecraft engineer for the evaluation of launch-window constraints or of attitude accuracies for different attitude sensor configurations.

Abstract

Abstract is not available.

Citation format

SHUSTER, M.; OH, S. Three-axis attitude determination from vector observations. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1981, 4: 70–77.