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Showing 1 to 5 of 5 for “"Aircraft System Identification"”.

  1. Aircraft System Identification Approach for Control Surface Fault Diagnosis

    … of effectiveness on a small, fixed-wing research aircraft. The work considers several real-time system identification methods to estimate changes in control effectiveness and provide fault information to a fault-tolerant control allocation framework. A baseline aero-propulsive model for an …

    vt Repository record for Aircraft System Identification Approach for Control Surface Fault Diagnosis (opens in a new tab)

  2. Online Aircraft System Identification Using a Novel Parameter Informed Reinforcement Learning Method

    … learning neural networks for online aircraft system identification of multiple similar linear systems, such as all fixed wing aircraft. This approach, termed Parameter Informed Reinforcement Learning (PIRL), dictates that reinforcement learning neural networks should be trained using …

    embry-riddle Repository record for Online Aircraft System Identification Using a Novel Parameter Informed Reinforcement Learning Method (opens in a new tab)

  3. Advances in Aero-Propulsive Modeling for Fixed-Wing and eVTOL Aircraft Using Experimental Data

    Small unmanned aircraft and electric vertical takeoff and landing (eVTOL) aircraft have recently emerged as vehicles able to perform new missions and stimulate future air transportation methods. This dissertation presents several system identification research advancements for these modern aircraft

    vt Repository record for Advances in Aero-Propulsive Modeling for Fixed-Wing and eVTOL Aircraft Using Experimental Data (opens in a new tab)

  4. Accelerating Practical Engineering Design Optimization with Computational Graph Transformations

    … design workflows for large-scale engineered systems, such as aircraft. However, despite remarkable theoretical progress in advanced optimization methods in recent decades, practical industry adoption of such methods lags far behind. This thesis identifies the root causes of this …

    mit Repository record for Accelerating Practical Engineering Design Optimization with Computational Graph Transformations (opens in a new tab)

  5. Identification of Unsteady Flight Dynamic Models and Model-based Wind Estimation with Flight Test Validation

    … boundary layer (ABL). Small, low-cost, uncrewed aircraft (drones) can be used to measure wind and a distribution of these vehicles could potentially provide measurements with much greater density and resolution, in both space and time, than current methods allow. To measure wind, a drone could be …

    vt Repository record for Identification of Unsteady Flight Dynamic Models and Model-based Wind Estimation with Flight Test Validation (opens in a new tab)