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A novel optimal approach for control law of multi-rate systems with different rate operations

Alireza Roosta

Alireza Roosta

Shiraz University of Technology, Power and Control DepartmentShiraz, Iran
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Roosta, Alireza
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Alireza Soltanimehr

Alireza Soltanimehr

Shiraz University of Technology, Power and Control DepartmentShiraz, Iran
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Soltanimehr, Alireza
  
15. Apr. 2022
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Artikel-Kategorie: Article
Online veröffentlicht: 15. Apr. 2022
Eingereicht: 18. Aug. 2021
DOI: https://doi.org/10.2478/ijssis-2022-0001
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© 2022 Alireza Roosta et al., published by Sciendo
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

Figure 1

Multipurpose system: (A) Simple view of a multi-rate system, (B) Decomposed form of switching, (C) Vectored decomposed form.
Multipurpose system: (A) Simple view of a multi-rate system, (B) Decomposed form of switching, (C) Vectored decomposed form.

Figure 2

Block diagram of simulated multi-rate guided missile.
Block diagram of simulated multi-rate guided missile.

Figure 3

The path of the missile and the target on the xyz coordinate.
The path of the missile and the target on the xyz coordinate.

Figure 4

Missile–target engagement in x–y coordinate.
Missile–target engagement in x–y coordinate.

Figure 5

Missile–target engagement in x–z coordinate.
Missile–target engagement in x–z coordinate.

Figure 6

Missile–target engagement in y–z coordinate.
Missile–target engagement in y–z coordinate.

Figure 7

Acceleration command in x screen over time.
Acceleration command in x screen over time.

Figure 8

Acceleration command in y screen over time.
Acceleration command in y screen over time.

Figure 9

Acceleration command in z screen over time.
Acceleration command in z screen over time.
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