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    General Extended State Observer-Based Robust Integral of Signum of Error Controller for Active Flutter Suppression for Aeroelastic System 

    Source: Journal of Computational and Nonlinear Dynamics:;2024:;volume( 019 ):;issue: 008:;page 81002-1
    Author(s): Sharma, Balraj; Agrawal, Pooja; Misra, Ajay
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The paper presents a robust integral of signum of error (RISE) controller for active suppression of flutter of a two-dimensional airfoil, and it is integrated with a general extended state observer (GESO). Toward this, ...
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    Optimized Uncertainty and Disturbance Estimator Based Robust Controller for Micro Aerial Vehicle 

    Source: Journal of Computational and Nonlinear Dynamics:;2022:;volume( 017 ):;issue: 011:;page 111006
    Author(s): Dixit, Abhishek;Agrawal, Pooja;Misra, Ajay
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The work presents optimized uncertainty and disturbance estimator (UDE) based robust controller to achieve the fixed wing micro-aerial vehicle (MAV) longitudinal and lateral stability. In the proposed control methodology, ...
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    Flow Field Characterization and Visualization of Grid Fin Subsonic Flow 

    Source: Journal of Fluids Engineering:;2019:;volume( 141 ):;issue: 010:;page 101401
    Author(s): Tripathi, Manish; Sucheendran, Mahesh M.; Misra, Ajay
    Publisher: American Society of Mechanical Engineers (ASME)
    Abstract: Grid fins are unconventional control surfaces consisting of an outer frame supporting an inner grid of intersecting planar surfaces. Although afflicted with higher drag, these have been credited for their enhanced lifting ...
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    Extended State Observer-Based Optimized Terminal Sliding Mode Fault-Tolerant Controller for Wing-Rock Suppression in Subsonic Incompressible Flow 

    Source: Journal of Computational and Nonlinear Dynamics:;2025:;volume( 020 ):;issue: 006:;page 61006-1
    Author(s): Sharma, Balraj; Agrawal, Pooja; Misra, Ajay
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents an adaptive fault-tolerant controller using terminal sliding mode theory to control the wing-rock motion in a slender delta wing. The governing equations of motion of have been obtained using the unsteady ...
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