SBIR/STTR Research Award
Integrated Sensing and Control of Aeroelastic Deformation (ISCAD) Toolbox
Award amount
$100,000Program and phase
STTR · Phase IAward year
2006Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- Tao Of Systems Integration Inc
- Proposal award date
- 2006-01-20
- Contract end date
- 2007-01-22
- UEI
- EW9UC5TFJ5L8
- Solicitation number
- Not reported
- Topic code
- T2.02
Research abstract
An Integrated Sensing and Control of Aeroelastic Deformation (ISCAD) Toolbox is proposed. Specif-ically, this toolbox will provide a methodology, both hardware and software, that serves to compensate for uncommanded de?ections of ?ight systems. This toolbox is meant to augment existing procedures for design of both aircraft and autopilots by providing additional capabilities that address aspects unique to for aeroelastic control. The sensors are provided by the ?ow and loads measuring systems pioneered by Tao Systems while the control synthesis builds upon expertise at the University of Florida in ?exible -wing aeroelasticity. The approach integrates state--of--the -art sensing capability with advanced control synthesis systems. In this way, a collaborative partnership is formed that is ideally suited to develop the ISCAD Toolbox.
Technology keywords
Not reported
Other awards by this recipient
Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.
- Balloon-Based Disturbance Measurements in the Upper Atmosphere
- Low-Cost, Low-Power Sensor For In-Flight Unsteady Aerodynamic Force and Moment Estimation
- Balloon-Based Disturbance Measurements in the Upper Atmosphere
- Robust Sensor for In-Flight Flow Characterization
- Distributed, Passivity-Based, Aeroservoelastic Control (DPASC) of Structurally Efficient Aircraft in the Presence of Gusts
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Vorticity State Estimation For Aeroelastic Control
- Embedded Fiber Optic Shape Sensing for Aeroelastic Wing Components
- A Reusable, Oxidizer-Cooled, Hybrid Aerospike Rocket Motor for Flight Test
- GVT-Based Ground Flutter Test without Wind Tunnel
- Online Real-Time Tribology Failure Detection System
Research funding history
46 SBIR/STTR records share this UEI (1995–2018). Reported award amounts total $13,652,764. Reported amounts are not federal obligations.
Phases: Phase I, Phase II
Agencies: National Aeronautics and Space Administration, Department of Defense