Biomedical Engineering Reference
In-Depth Information
The optimal control for Problem 4.4 (for the rigid-body model) is
given by Eq. (3.40) and, accordingly,
V
U
.
u
0
(t)
˜
=−
U
for
0
≤
t
≤
T
=
(4)
The corresponding time history of the coordinate
x
is given by
1
2
Ut
2
x
0
(t)
=
Vt
−
for
0
≤
t
≤
T.
(5)
The numerical results will be presented below for
V
=
10 m
/
s
(
=
36 km
/
h
).
(6)
This is a typical velocity for vehicle crashes. To calculate the deceleration
time of the object in the rigid-body model, substitute 10 m
/
sfor
V
and
400 m
/
s
2
for
U
into the expression of (4) for
T
. This yields
T
=
25 ms
.
(7)
In the case under consideration, the response characteristics satisfy
Assumptions 1 - 3.
The optimal behavior of the system is shown in Figs. 4.2 - 4.6.
Figure 4.2 shows the optimal control force
u
0
(t)
for Problem 4.2.
The
y
0
(t)
are
plotted in Figs. 4.3, 4.4, and 4.5, respectively. On the time interval
0
optimal
time
histories
x
=
x
0
(t)
,
ξ
=
ξ
0
(t)
,and
y
=
≤
≤
T
, the function
x
0
(t)
is defined by (5) and the functions
ξ
0
(t)
and
y
0
(t)
are defined by Eqs. (4.35) and (4.44), respectively.
t
20
0
-20
-40
0
10
20
30
Time (ms)
FIGURE 4.2
Optimal control
u
0
(t)
for Problem 4.2.
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