Yh. Kwon, Experimental simulation of an airborne movement: Applicability of the bodysegment parameter estimation methods, J AP BIOMEC, 17(3), 2001, pp. 232-240
The purpose of this study was twofold: (a) to investigate the effect of the
method of body segment parameter (BSP) estimation on the accuracy of the e
xperimental simulation of a complex airborne movement; and (b) to assess th
e applicability of selected BSP estimation methods in the experimental simu
lation. It was hypothesized that different BSP estimation methods would pro
vide different simulation results. A sensitivity analysis was performed to
identify the BSP items and segments responsible for the inter-method differ
ences in the simulation accuracy. The applicability of the estimation metho
ds was assessed based on the simulation results and the number of anthropom
etric parameters required. Ten BSP estimation methods classified into 3 gro
ups (4 cadaver-based, 4 gamma mass scanning-based, and 2 geometric) were em
ployed in a series of experimental simulations based on 9 double-somersault
-with-full-twist H-bar dismounts performed by 3 male college gymnasts. The
simulated body orientation angles were compared with the corresponding obse
rved orientation angles in computing the simulation errors. The inclination
and twist simulation errors revealed significant (p < .05) differences amo
ng the BSP estimation groups and methods. It was concluded that: (a) the me
thod of BSP estimation significantly affected the simulation accuracy, and
more individualized BSP estimation methods generally provided more accurate
simulation results; (b) the mass items, and the lower leg and thorax/abdom
en were more responsible for the intermethod differences in the simulation
accuracy than other BSP items and segments, respectively; (c) the ratio met
hods and the simple regression methods were preferable in simulation of the
somersaulting motion due to the fewer anthropometric parameters required;
(d) the geometric models and the cadaver-based stepwise regression method w
ere superior to the other methods in the simulation of the complex airborne
motion with twist.