1983
DOI: 10.1115/1.3167078
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Spacecraft Dynamics

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Cited by 232 publications
(77 citation statements)
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“…Once the displacement trajectories for a minimum of three noncolinear points were known, the bone's complete 3D rotation matrix and translation trajectory were calculated [21,43]. The rotation matrix was simplified to three Cardan rotation angles using an xyz body-fixed rotation Quantitative J-sign* (present) 7 0…”
Section: Methodsmentioning
confidence: 99%
“…Once the displacement trajectories for a minimum of three noncolinear points were known, the bone's complete 3D rotation matrix and translation trajectory were calculated [21,43]. The rotation matrix was simplified to three Cardan rotation angles using an xyz body-fixed rotation Quantitative J-sign* (present) 7 0…”
Section: Methodsmentioning
confidence: 99%
“…For data presentation, the orientation matrices were simplified to orientation angles (Fig. 4) based on an xyz body-fixed rotation sequence (22,23).…”
Section: Methodsmentioning
confidence: 99%
“…In the development presented in the subsequent sections, the right-handed Cartesian coordinate systems oxyz and O 2 x 2 y 2 z 2 are used as an inertial reference system and a body-fixed reference system, respectively; the space-three-angles x-y-z defined in the Ref. [16], are used as the orientation angles of involved bodies.…”
Section: General Theorems and Steps Of The Proposed Methodsmentioning
confidence: 99%