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International Journal of Differential Equations
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International Journal of Differential Equations
/
2009
/
Article
/
Fig 11
/
Research Article
Oscillation Susceptibility Analysis of the ADMIRE Aircraft along the Path of Longitudinal Flight Equilibriums in Two Different Mathematical Models
Figure 11
Oscillations when
𝛿
𝑒
=
−
0
.
0
4
6
7
8
[
r
a
d
]
=
−
2
.
6
8
1
∘
→
𝛿
𝑒
=
−
0
.
0
5
[
r
a
d
]
=
−
2
.
8
6
6
∘
and the starting point is
𝛼
1
=
0
.
0
8
6
9
7
4
2
[
r
a
d
]
=
4
.
9
8
5
∘
;
𝑞
1
=
0
[
r
a
d
/
s
e
c
]
;
𝜃
1
=
0
.
1
5
9
3
2
9
[
r
a
d
]
=
9
.
1
3
3
∘
.
(a)
(b)
(c)