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Showing 1 to 5 of 5 for “"Control Saturation"”.

  1. Gradient projection anti-windup scheme

    It is a well-recognized fact that control saturation affects virtually all practical control systems. It leads to controller windup, which degrades/limits the system's closed-loop performance, and may cause catastrophic failures if it induces instability. Anti-windup compensation is one of two main …

    mit Repository record for Gradient projection anti-windup scheme (opens in a new tab)

  2. Terminal control of a variable-stability slender reentry vehicle

    Various terminal control schemes are applied to a proposed slender reentry vehicle, controlled by two separately-articulating flaps. The flap deflections are summarized as symmetric and asymmetric flap deflections; the former manipulates the drag, lift-curve slope, and static margin; the latter …

    mit Repository record for Terminal control of a variable-stability slender reentry vehicle (opens in a new tab)

  3. Adaptive Flight Control in the Presence of Input Constraints

    … and stability of these systems. Adaptive control offers a useful means for controlling systems in the presence of uncertainties. However, very often adaptive controllers require more control effort than the actuator limits allow. In this thesis the original work of others on single input …

    vt Repository record for Adaptive Flight Control in the Presence of Input Constraints (opens in a new tab)

  4. Evacuation Distributed Feedback Control and Abstraction

    In this dissertation, we develop feedback control strategies that can be used for evacuating people. Pedestrian models are based on macroscopic or microscopic behavior. We use the macroscopic modeling approach, where pedestrians are treated in an aggregate way and detailed interactions are …

    vt Repository record for Evacuation Distributed Feedback Control and Abstraction (opens in a new tab)

  5. A Comparison of Two Methods Used to Deal with Saturation of Multiple, Redundant Aircraft Control Effectors

    … of two methods to deal with allocating controls for unattainable moments in an aircraft was performed using a testbed airframe that resembled an F/A-18 with a large control effector suite. The method of preserving the desired moment direction to deal with unattainable moments is …

    vt Repository record for A Comparison of Two Methods Used to Deal with Saturation of Multiple, Redundant Aircraft Control Effectors (opens in a new tab)