
14
104,102106,406
−−
×× +v=t
a1p1
(s) 
(1)
 
0,0680,967
a2p2
v=t (s) 
(2)
 
Using these equations we can obtain estimates of 
the loft time (t
pi
) from the variables measured from 
the  accelerometer signal (v
ai
). 
The loft time relative error associated with each 
of the algorithms i was determined for each jump j 
(δ
εij
), taking as “real” loft times the values measured 
from the force platform signal(t
pj
). 
(
)
1,2 1,... 60
pp
jij
ε
ij
p
j
tt
δ =,i=;j=,
t
−
    (3) 
The accuracy of the algorithms was assessed by 
determining the corresponding average loft time 
relative errors: 
δ
εi
=
∑
δ
εij
n
,i= 1,2 j=1,..., 60
 
(4)
 
The results led to relative errors of 7,0% for the 
first algorithm and 2,9% for the second algorithm 
Taking as reference the mean loft time determined  
for the set of 60 jumps with the regression equations 
(1) and (2) these relative errors correspond to 32 ms 
and 13 ms, respectively.  
Both algorithms are also affected by a common 
base error of 0.1% which is characteristic of the 
acquisition unit and inversely proportional to its 
sampling rate. 
Usually, when the force platform is used to 
determine the loft time an associated error of 0,5% is 
introduced because the algorithm is susceptible of 
the parameters chosen by the user as the initial and 
final points of the flight stage. In contrast, the 
algorithms we propose are automatic. 
5 CONCLUSIONS 
The time interval between the minimum acceleration 
value of the flying stage and the maximum 
acceleration value of the landing stage is the best of 
the two devised measures, showing a good 
correlation with the real loft times (r=0.933 and 
δ
ε
.=2,9%). 
Although associated with errors, these 
preliminary results indicate that these algorithms are 
good alternative methods for the computation of loft 
time, taking advantage of the use of an 
accelerometer instead of a force platform, which is 
more expensive and less portable.  
In addition to the flight time other parameters 
used to assess the performance of the jump can be 
found on the acceleration signal, such as the height 
of the jump. Furthermore, information on the 
dynamic behaviour of the jumper, namely during the 
flight stage can also be obtained from the 
acceleration signal, which is impossible to study 
with only the vertical force signal.  
In the future, we plan to study the load 
distribution between inferior members during the 
take-off and landing stages by combining 
acceleration and force analysis and study the on-
flight behaviour of the jumper. 
REFERENCES 
Dowling J., Vamos, L., 1993, J., Identification of Kinetic 
and Temporal Factors Related to Vertical Jump 
Performance, Applied Biomechanics, 9. 
Linthorne, N. P., 2001, Analysis of standing vertical jumps 
using a force platform, Am. Journal of Phys., 69 (11). 
Hassan R., Begg R. K., Khandoker A. H., Stokes R., 2006, 
Automated Recognition of Human Movement in Stress 
Situations, Proceedings of the 2
nd
 Internationsl 
Workshop on Biosignal Procesing and Classification – 
BPC 2006, INSTICC Press. 
Silva H., Gamboa H., Viegas V., Fred A., 2005, Wireless 
Physiologic Data Acquisition Platform., 2005. 
Proceedings of the 5
th
 Conference on 
Telecomunications Confele. 
http://www.plux.info 
http://www.amtiweb.com/bio/force_platforms.htm 
Proakis J. G., Manolakis D., 1995, Digital Signal 
Processing: Principles, Algorithms and Applications, 
Pearson US Import & PHIPEs, 3
rd
 International 
Edition. 
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