(a)
(b)
(c)
(d)
Figure 14:
Transfer from
𝛼
1
=
0
.
0
7
8
6
6
9
7
[
r
a
d
]
=
4
.
5
0
9
∘
;
𝑞
1
=
0
[
r
a
d
/
s
]
;
𝜃
1
=
−
0
.
4
2
8
8
3
2
[
r
a
d
]
=
−
2
4
.
5
8
∘
into a state which is appropriate for the touch-down moment
𝜃
−
𝛼
=
0
and
𝜃
>
0
(
𝜃
small).
