Tao Of Systems Integration Inc

Company Information
Address 1100 Exploration Way
HAMPTON, VA, 23666-6264

http://www.taosystems.us

Information

DUNS: 840701445

# of Employees: 5


Ownership Information

HUBZone Owned: N

Socially and Economically Disadvantaged: Y

Woman Owned: N



Award Charts




Award Listing

  1. Low-Cost, Low-Power Sensor For In-Flight Unsteady Aerodynamic Force and Moment Estimation

    Amount: $124,999.00

    Tao Systems and University of Minnesota propose to develop a sensor system providing sectional aerodynamic forces and moments with fast response, low volume/size/power requirements for ease of install ...

    SBIRPhase I2017National Aeronautics and Space Administration
  2. Distributed, Passivity-Based, Aeroservoelastic Control (DPASC) of Structurally Efficient Aircraft in the Presence of Gusts

    Amount: $750,000.00

    Control of extremely lightweight, long endurance aircraft poses a challenging aeroservoelastic (ASE) problem due to significantly increased flexibility, and aerodynamic, structural, and actuator nonli ...

    STTRPhase II2015National Aeronautics and Space Administration
  3. Robust Sensor for In-Flight Flow Characterization

    Amount: $125,000.00

    Tao Systems proposes to develop a sensor system providing quantitative in-flight boundary layer flow characterization with fast response, low volume, minimal intrusion, high accuracy and robustness to ...

    SBIRPhase I2015National Aeronautics and Space Administration
  4. Distributed, Passivity-Based, Aeroservoelastic Control (DPASC) of Structurally Efficient Aircraft in the Presence of Gusts

    Amount: $125,000.00

    Control of extremely lightweight, long endurance aircraft poses a challenging aeroservoelastic (ASE) problem due to significantly increased flexibility, and aerodynamic, structural, and actuator nonli ...

    STTRPhase I2014National Aeronautics and Space Administration
  5. Vorticity State Estimation For Aeroelastic Control

    Amount: $125,000.00

    Flight control, structural reliability, and efficiency depend critically on the ability to assess the time-accurate unsteady aerodynamic loads and moments for each lifting surface under nominal and ad ...

    STTRPhase I2012National Aeronautics and Space Administration
  6. Robust Aeroservoelastic Control Utilizing Physics-Based Aerodynamic Sensing

    Amount: $750,000.00

    New aircraft designs depend on an integrated active approach to flight control, flutter suppression and structural mode attenuation to meet desired handling quality performance and gust load alleviati ...

    STTRPhase II2012National Aeronautics and Space Administration
  7. High Frequency Measurements in Shock-Wave/Turbulent Boundary-Layer Interaction at Duplicated Flight Conditions

    Amount: $750,000.00

    Large amplitude, unsteady heating loads and steep flow gradients produced in regions of shock-wave/turbulent boundary-layer interaction (SWTBLI) pose a serious and challenging problem for designers of ...

    SBIRPhase II2012National Aeronautics and Space Administration
  8. Robust Aeroservoelastic Control Utilizing Physics-Based Aerodynamic Sensing

    Amount: $100,000.00

    New aircraft designs depend on an integrated active approach to flight control, flutter suppression and structural mode attenuation to meet desired handling quality performance and gust load alleviati ...

    STTRPhase I2011National Aeronautics and Space Administration
  9. Biomimetic Approach for Accurate, Real-Time Aerodynamic Coefficients

    Amount: $100,000.00

    Aerodynamic and structural reliability and efficiency depends critically on the ability to accurately assess the aerodynamic loads and moments for each lifting surface. A thin-film, flight-worthy sens ...

    SBIRPhase I2011National Aeronautics and Space Administration
  10. High Frequency Measurements in Shock-Wave/Turbulent Boundary-Layer Interaction at Duplicated Flight Conditions

    Amount: $99,262.00

    Large amplitude, unsteady heating loads and steep flow gradients produced in regions of shock-wave/turbulent boundary-layer interaction (SWTBLI) pose a serious and challenging problem for designers o ...

    SBIRPhase I2011National Aeronautics and Space Administration

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