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Power System Analysis and Design (MindTap Course List)
6th Edition
ISBN: 9781305632134
Author: J. Duncan Glover, Thomas Overbye, Mulukutla S. Sarma
Publisher: Cengage Learning
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Question
Is the uncontrolled, open loop system?
a.unstable
b.not asymptotically stable
c.asymptotically stable
d.unstable
![The longitudinal dynamics of the aircraft is defined by:
x = Ax+Bu, A=
B=B₁ = [0
B = BE = [0
For measurements
C=C₁ = [1
Ca
C=C₁ = [0
O a.
0
0
0
0
0
0
-0.05
0
0.05
-0.3
With the thrust only input or the elevator only input, the corresponding B matrices are:
unstable
1 0 0 0],
0 1 0 0]
0.001 0001
0 0 -2 -0.1]
C=C₂ = [0
Is the uncontrolled, open loop system?
d. unstable
1
-0.2
0
0
0
0
0
1
−1
1
of either the altitude, speed or pitch angle, the corresponding C matrices are:
0 0 0 0],
O b. not asymptotically stable
O c. asymptotically stable
-1
0.1
0
-1
-0.7
"
y = Cx](https://content.bartleby.com/qna-images/question/df6bbd7c-5d08-4329-80df-c691787490e9/70ab3cc4-87ba-4b72-baa2-82fe83f652b6/n0abt7q_thumbnail.png)
Transcribed Image Text:The longitudinal dynamics of the aircraft is defined by:
x = Ax+Bu, A=
B=B₁ = [0
B = BE = [0
For measurements
C=C₁ = [1
Ca
C=C₁ = [0
O a.
0
0
0
0
0
0
-0.05
0
0.05
-0.3
With the thrust only input or the elevator only input, the corresponding B matrices are:
unstable
1 0 0 0],
0 1 0 0]
0.001 0001
0 0 -2 -0.1]
C=C₂ = [0
Is the uncontrolled, open loop system?
d. unstable
1
-0.2
0
0
0
0
0
1
−1
1
of either the altitude, speed or pitch angle, the corresponding C matrices are:
0 0 0 0],
O b. not asymptotically stable
O c. asymptotically stable
-1
0.1
0
-1
-0.7
"
y = Cx
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- Power System Analysis and Design (MindTap Course ...Electrical EngineeringISBN:9781305632134Author:J. Duncan Glover, Thomas Overbye, Mulukutla S. SarmaPublisher:Cengage Learning
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Power System Analysis and Design (MindTap Course ...
Electrical Engineering
ISBN:9781305632134
Author:J. Duncan Glover, Thomas Overbye, Mulukutla S. Sarma
Publisher:Cengage Learning