Physics
Scientific paper
Mar 1982
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1982kosis..20..184b&link_type=abstract
Kosmicheskie Issledovaniia, vol. 20, Mar.-Apr. 1982, p. 184-190. In Russian.
Physics
Error Analysis, Kinematic Equations, Strapdown Inertial Guidance, Angular Velocity, Block Diagrams, Quaternions
Scientific paper
Error equations are derived for the solution of kinematic equations by the quaternion method. It is shown that all the error sources can be reduced to an equivalent error of the primary information. Examples of determining solutions of the kinematic equations and their errors are considered, with particular attention given to the use of angular velocity as the primary information (a case typical for spacecraft attitude measurements). The present study is also pertinent to the formulation of kinematic equations for strapdown inertial navigation.
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