Aircraft Flight Envelope Identification through On-Board Model Based Estimation

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$99,881.00
Award Year:
2009
Program:
SBIR
Phase:
Phase I
Contract:
NNX09CE91P
Award Id:
90787
Agency Tracking Number:
085399
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
34 Lexington Avenue, Ewing, NJ, 08618
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
096857313
Principal Investigator:
Jefrfrey Keller
Principal Investigator
(609) 538-0444
jeff@continuum-dynamics.com
Business Contact:
Barbara Agans
Business Official
(609) 538-0444
barbara@continuum-dynamics.com
Research Institute:
n/a
Abstract
To improve aviation safety with anticipated growth in capacity, it is necessary to develop flight control technologies that enable safe operations as anomalous conditions occur. These developments are particularly important to reduce fatal loss of control accidents due to aircraft degradation and abrupt aerodynamic changes including upsets. It is necessary to develop methods to identify and characterize anomalies in flight, as well as to estimate the impacts on the flight envelope and the ability to effect control forces for recovery and/or flight planning to achieve safe landing. An approach to identify anomalies including aerodynamic upsets based on model-based fault detection methods will be combined with physics-based models to assess the impact on the aircraft flight envelope and controllability. These tools will permit off-line analysis and will facilitate the development of on-board guidance and control algorithms to support NASA goals for greater aircraft resiliency during adverse flight conditions. In Phase I, development and demonstration of a generalized system architecture to identify and assess the effects of aircraft anomalies will be performed, which builds upon previous work toward model-based aircraft upset detection. Phase I demonstrations will include simulation evaluation for a generic transport aircraft and test demonstration for a small unmanned aircraft.

* information listed above is at the time of submission.

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