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m
=
F
L
+
F
drag
,
R
¨
z
F
R
−
F
drag
,
L
−
θ
=
F
R
−
F
drag
,
R
r
(6.23)
1
2
mr
2
F
L
+
F
drag
,
L
−
where:
F
drag
,
L
=
k
drag
v
L
|
v
L
|
F
drag
,
R
=
k
drag
v
R
|
v
R
|
(6.24)
r
θ
r
θ
v
L
=˙
z
−
v
R
=˙
z
+
with
k
drag
=
11 kg/m being the drag coefficient in the normal operating conditions,
z
the total covered distance,
θ
the angular
velocity. The system can be controlled using the available control inputs
F
L
and
F
R
,
that are the forces acting on the left and the right wheel, which have velocities
v
L
and
v
r
, respectively.
By considering the state vector
x
z
the linear velocity,
˙
θ
the yaw angle and
=
F
L
F
R
T
,
and embedding the nonlinearities in the parameters, (
6.23
) can be put in the following
form:
⎛
⎝
=
z
θ θ
T
, the input vector
u
˙
z
⎞
⎠
=
⎛
⎝
⎞
⎠
⎛
⎝
⎞
⎠
+
x
1
(
˙
t
)
0
1
0
0
x
1
(
t
)
B
u
1
(
x
2
(
˙
t
)
0
a
22
(
x
2
,
x
4
)
0
a
24
(
x
2
,
x
4
)
x
2
(
t
)
t
)
(6.25)
x
3
(
˙
t
)
0
0
0
1
x
3
(
t
)
u
2
(
t
)
x
4
(
˙
t
)
0
a
42
(
x
2
,
x
4
)
0
a
44
(
x
2
,
x
4
)
x
4
(
t
)
with:
01
T
/
m
0
−
2
/(
mr
)
B
=
(6.26)
01
/
m
02
/(
mr
)
⎧
⎨
−
2
k
drag
x
2
/
m
2
≥ |
rx
4
|
−
2
rk
drag
x
4
/
m
−
rx
4
<
x
2
<
rx
4
a
22
(
x
2
,
x
4
)
=
(6.27)
2
rk
drag
x
4
/
mrx
4
<
x
2
<
−
rx
4
⎩
2
k
drag
x
2
/
mx
2
≤ |
rx
4
|
⎧
⎨
2
k
drag
r
2
x
4
/
−
m
2
≥ |
rx
4
|
−
2
rk
drag
x
2
/
m
−
rx
4
<
x
2
<
rx
4
a
24
(
x
2
,
x
4
)
=
(6.28)
2
rk
drag
x
2
/
mrx
4
<
x
2
<
−
rx
4
⎩
2
k
drag
r
2
x
4
/
m
2
≤ |
rx
4
|
⎧
⎨
−
4
k
drag
x
4
/
mx
2
≥ |
rx
4
|
−
4
k
drag
x
2
/(
mr
)
−
rx
4
<
x
2
<
rx
4
a
42
(
x
2
,
x
4
)
=
(6.29)
4
k
drag
x
2
/(
mr
)
rx
4
<
x
2
<
−
rx
4
⎩
4
k
drag
x
4
/
mx
2
≤ |
rx
4
|
⎧
⎨
−
4
k
drag
x
2
/
mx
2
≥ |
rx
4
|
−
4
rk
drag
x
4
/
m
−
rx
4
<
x
2
<
rx
4
a
44
(
x
2
,
x
4
)
=
(6.30)
⎩
4
rk
drag
x
4
/
mrx
4
<
x
2
<
−
rx
4
4
k
drag
x
2
/
mx
2
≤ |
rx
4
|
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