Flight control for the F-8 oblique wing research aircraft

Enns, Dale; Bugajski, Dan; Klepl, Martin J.

doi:10.1109/37.1879

Cited by 7 publications

(3 citation statements)

References 4 publications

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“…This condition (16), which is applied to the reordered system, remains valid as both GB and differ solely in row and column reordering while retaining the same absolute value for the determinant.…”

Section: Design Of Sliding Surfacesmentioning

confidence: 99%

Resilient Sliding Mode Control via Direct Pole Placement Technique for Large Scale Systems

Hnnie Williams

2023

IJRITCC

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This paper introduces an innovative method for determining the switching surface within an equivalent pole placement control framework designed specifically for multivariable systems. Moreover, it showcases adaptability across both minimum phase and non-minimum phase systems. The sliding mode control system offers significant flexibility in shaping the closed-loop eigenvalues, providing considerable freedom in customizing the system's characteristics. The formulation of the sliding surface plays a crucial role in defining the performance features of the control system, as the representative point of the system is constrained to follow a predetermined switching surface. Researchers are actively addressing the pole assignment problem within sliding mode control, presenting a unique geometric approach for designing sliding surfaces. This contribution introduces a fresh perspective to the domain of control system design, and the inclusion of numerical examples serves to highlight the simplicity and effectiveness of the proposed method.

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Section: Design Of Sliding Surfacesmentioning

confidence: 99%

Resilient Sliding Mode Control via Direct Pole Placement Technique for Large Scale Systems

Hnnie Williams

2023

IJRITCC

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“…During the flight of aircraft, it is influenced strongly by the aerodynamic coupling, the inertial coupling and the kinematic coupling, synchronously. In such cases, some scholars(such as Deng et al (2010), Zhou (1995), and Enns et al (1988)) have already conducted researches on the decoupling control problems of aircraft. To investigate the effectiveness of the proposed control method, we research a flight control example based on the hypersonic vehicle.…”

Section: Flight Control Examplementioning

confidence: 99%

H based decoupling tracking control of hypersonic vehicle

Lan

Wang

Liu

et al. 2014

IFAC Proceedings Volumes

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“…In this section, the robust performance of the gain scheduled system is defined. The definition used here deliberately resembles that of Doyle et al (1982) because of its practical utility (Enns, 1987;Enns and Bugajski, 1987). However, we deviate slightly with our definition.…”

Section: A Scheduled System Robust Performancementioning

confidence: 99%