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Showing 1 to 9 of 9 for “"control effector"”.

  1. A Comparison of Control Allocation Methods for the F-15 ACTIVE Research Aircraft Utilizing Real-Time Piloted Simulations

    A comparison of two control allocation methods is performed utilizing the F-15 ACTIVE research vehicle. The control allocator currently implemented on the aircraft is replaced in the simulation with a control allocator that accounts for both control effector positions and rates. Validation of the …

    vt Repository record for A Comparison of Control Allocation Methods for the F-15 ACTIVE Research Aircraft Utilizing Real-Time Piloted Simulations (opens in a new tab)

  2. 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 …

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  3. Investigation of Control Effectors for Ducted Fan VTOL UAVs

    … order of Re = 0.96 x 106 to 4.6 x 106. Various control effectors were mounted to the vehicle and tested for maximum control authority to reduce the nose-up pitch moment created during forward flight or with crosswinds present. Static and wind tunnel tests were conducted to measure each control

    vt Repository record for Investigation of Control Effectors for Ducted Fan VTOL UAVs (opens in a new tab)

  4. Effects of Duct Lip Shaping and Various Control Devices on the Hover and Forward Flight Performance of Ducted Fan UAVs

    … on the interior of the duct lip surface. Control vanes positioned aft of the duct were tested as the primary attitude control for the vehicle. An empirical control vane model was created based on the static data for the control vanes, and it was applied to wind tunnel test results to …

    vt Repository record for Effects of Duct Lip Shaping and Various Control Devices on the Hover and Forward Flight Performance of Ducted Fan UAVs (opens in a new tab)

  5. Aerodynamic Analysis of Variable Geometry Raked Wingtips for Mid-Range Transonic Transport Aircraft

    … a variable geometry raked wingtip novel control effector (VGRWT/NCE) was studied to determine the aerodynamic performance benefits over an untreated wingtip. The Boeing SUGAR design employing a truss-braced wing was selected as the baseline. Vortex lattice method (VLM) and computational …

    vt Repository record for Aerodynamic Analysis of Variable Geometry Raked Wingtips for Mid-Range Transonic Transport Aircraft (opens in a new tab)

  6. Bhlhe40: Required For Tumor Microenvironment Remodeling and Immune Checkpoint Therapy Efficacy

    … effect on specific immune checkpoints to control effector T cell functions(Pardoll, 2012). This therapy allows for the modulation of anti-tumor responses through the use of monoclonal antibodies, such as anti-CTLA-4 or anti-PD-1 that block the receptors from binding with their ligands, …

    uthsc Repository record for Bhlhe40: Required For Tumor Microenvironment Remodeling and Immune Checkpoint Therapy Efficacy (opens in a new tab)

  7. Design, Development, and Analysis of a Morphing Aircraft Model for Wind Tunnel Experimentation

    … can serve as a tool in learning to model, control, and fully exploit the potential of such vehicles. This work describes the design, development, and initial analysis of a wind tunnel model that combines large and small wing shape variations for fundamental research in modeling and control

    vt Repository record for Design, Development, and Analysis of a Morphing Aircraft Model for Wind Tunnel Experimentation (opens in a new tab)

  8. Aeroelastic Analysis of Truss-Braced Wing Aircraft: Applications for Multidisciplinary Design Optimization

    … aft relative to the wing with the aid of a Novel Control Effector (NCE) mechanism. Results show that the VGRWT can be swept judiciously to alter the bending-torsion coupling and the movement of the center of pressure of wing. Such behavior of the VGRWT is applied to both achieve the required roll …

    vt Repository record for Aeroelastic Analysis of Truss-Braced Wing Aircraft: Applications for Multidisciplinary Design Optimization (opens in a new tab)

  9. Structural Basis of Signal Transduction within Environmental Sensing PAS Regulated Ser/Thr Kinases

    … This process often relies on environmentally controlled <strong>PPIs</strong> (<strong>P</strong>rotein-<strong>P</strong>rotein <strong>I</strong>nteraction<strong>s</strong>) within a sensory domain that senses various stimuli and alters the functional activities of downstream effectors. …

    cuny-grad Repository record for Structural Basis of Signal Transduction within Environmental Sensing PAS Regulated Ser/Thr Kinases (opens in a new tab)