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Eigen-structure problem optimization for multirate, multi-input multi-output systems applied to a roll rate autopilot


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Figure 1

Single rate roll rate autopilot loop.
Single rate roll rate autopilot loop.

Figure 2

Multirate roll rate autopilot loop.
Multirate roll rate autopilot loop.

Figure 3

Input tracking by optimally designed output.
Input tracking by optimally designed output.

Figure 4

CRE error for inputs shown in Figure 3.
CRE error for inputs shown in Figure 3.

Calculated gains.

ki kp
2.5 0.39
2.5 0.48
2.5 0.41
2.5 0.506

Performance parameters after optimization

Feedback gain matrix k Performance value
k1 = 7.921 k1
k2 = 22.432
k3 = 26.29
k4 = 28.6301
4.69 JD1
9.501 JD2
1.429 k2
eISSN:
1178-5608
Language:
English
Publication timeframe:
Volume Open
Journal Subjects:
Engineering, Introductions and Overviews, other