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Tao Of Systems Integration Inc
UEI: EW9UC5TFJ5L8
# of Employees: 5
HUBZone Owned: No
Socially and Economically Disadvantaged: Yes
Woman Owned: No
Award Charts
Award Listing
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Balloon-Based Disturbance Measurements in the Upper Atmosphere
Amount: $750,000.00For prediction of hypersonic aerothermodynamics, knowledge of the relevant disturbance levels is required to determine transition locations in flight at the altitudes of interest. Tao Systems and Univ ...
STTRPhase II2018Department of Defense Air Force -
Low-Cost, Low-Power Sensor For In-Flight Unsteady Aerodynamic Force and Moment Estimation
Amount: $124,999.00Tao 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 -
Balloon-Based Disturbance Measurements in the Upper Atmosphere
Amount: $149,981.00For prediction of hypersonic aerothermodynamics, knowledge of the relevant disturbance levels is required to determine transition locations in flight at the altitudes of interest. Tao Systems and Univ ...
STTRPhase I2017Department of Defense Air Force -
Robust Sensor for In-Flight Flow Characterization
Amount: $125,000.00Tao 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 -
Distributed, Passivity-Based, Aeroservoelastic Control (DPASC) of Structurally Efficient Aircraft in the Presence of Gusts
Amount: $750,000.00Control 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 -
Distributed, Passivity-Based, Aeroservoelastic Control (DPASC) of Structurally Efficient Aircraft in the Presence of Gusts
Amount: $125,000.00Control 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 -
Vorticity State Estimation For Aeroelastic Control
Amount: $125,000.00Flight 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 -
Robust Aeroservoelastic Control Utilizing Physics-Based Aerodynamic Sensing
Amount: $750,000.00New 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 -
High Frequency Measurements in Shock-Wave/Turbulent Boundary-Layer Interaction at Duplicated Flight Conditions
Amount: $750,000.00Large 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 -
Robust Aeroservoelastic Control Utilizing Physics-Based Aerodynamic Sensing
Amount: $100,000.00New 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
