State Feedback Controllers with Operational Constraints
Fuente:
arXiv
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| Autore principale: | |
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| Natura: | Preprint |
| Pubblicazione: |
2025
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| Accesso online: | |
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| _version_ | 1866908673206386688 |
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| author | Lavretsky, Eugene |
| author_facet | Lavretsky, Eugene |
| contents | In this paper, a state feedback control design with min/max operational limiting constraints is developed for multi-input-multi-output linear time invariant systems. Specifically, servo-tracking control problems with input and output constraints are considered. For static servo-controllers, the output design limits are imposed component-wise on the system selected output, which is of the same dimension as the control input. For dynamic servo-controllers, operational constraints are applied to the system inputs and outputs. The proposed control solution also includes an anti-windup protection logic for dynamic servo-controllers with integral action. The developed method is based on the Nagumo Theorem for forward invariance, the Comparison Lemma for inclusion of input/output inequality constraints, and on the min-norm optimal controllers for synthesis. The derived design is similar and directly related to the method of Control Barrier Functions. Simulation trade studies are presented to illustrate benefits of the proposed control methodology for aerial flight critical systems. |
| format | Preprint |
| id |
arxiv_https___arxiv_org_abs_2511_19683 |
| institution | arXiv |
| publishDate | 2025 |
| record_format | arxiv |
| spellingShingle | State Feedback Controllers with Operational Constraints Lavretsky, Eugene Systems and Control In this paper, a state feedback control design with min/max operational limiting constraints is developed for multi-input-multi-output linear time invariant systems. Specifically, servo-tracking control problems with input and output constraints are considered. For static servo-controllers, the output design limits are imposed component-wise on the system selected output, which is of the same dimension as the control input. For dynamic servo-controllers, operational constraints are applied to the system inputs and outputs. The proposed control solution also includes an anti-windup protection logic for dynamic servo-controllers with integral action. The developed method is based on the Nagumo Theorem for forward invariance, the Comparison Lemma for inclusion of input/output inequality constraints, and on the min-norm optimal controllers for synthesis. The derived design is similar and directly related to the method of Control Barrier Functions. Simulation trade studies are presented to illustrate benefits of the proposed control methodology for aerial flight critical systems. |
| title | State Feedback Controllers with Operational Constraints |
| topic | Systems and Control |
| url | https://arxiv.org/abs/2511.19683 |