Variance-constrained control of maneuvering helicopters with sensor failure
Autor: | Tugrul Oktay, Cornel Sultan |
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Rok vydání: | 2012 |
Předmět: |
Flexibility (engineering)
Engineering Inertial frame of reference Mathematical model business.industry Mechanical Engineering Linear system Aerospace Engineering ComputerApplications_COMPUTERSINOTHERSYSTEMS Control engineering Maneuvering speed Banked turn Computer Science::Robotics Computer Science::Systems and Control Control theory Robustness (computer science) Design process ComputerSystemsOrganization_SPECIAL-PURPOSEANDAPPLICATION-BASEDSYSTEMS business |
Zdroj: | Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 227:1845-1858 |
ISSN: | 2041-3025 0954-4100 |
Popis: | This article presents the novel results obtained using variance-constrained controllers and maneuvering helicopters also when some helicopter sensors fail. For this purpose, complex, control oriented, and physics-based helicopter models are used. A nonlinear model of the helicopter, which includes blade flexibility, is first linearized around specific maneuvering flight conditions (i.e. level banked turn and helical turn). The resulting linearized models are used for the design of variance-constrained controllers (i.e. output and input variance-constrained controllers). Then, the robustness of the closed-loop systems with respect to modeling uncertainties (i.e. flight conditions and helicopter inertial parameters variations) is studied. Next, variance-constrained controllers are designed for these maneuvering helicopter models when some helicopter sensors fail. Several sensor failure cases are examined and robustness properties of the closed-loop systems with respect to modeling uncertainties are also examined. Limitations of the control design process due to the number and type of failed sensors are investigated as well. Finally, the possibility to adaptively switch between controllers in order to mitigate sensor failure is studied. |
Databáze: | OpenAIRE |
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