SBIR/STTR Research Award

IDENTIFICATION

Award identifier 2a4c3a8890ff6cfcb03662e33e78c97714ef8a34ae95f6a8ac6aef3b0c57aed1Awarding agency National Aeronautics and Space Administration

Award amount

$50,000

Program and phase

SBIR · Phase I

Award year

1985

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
Integrated Systems I
Proposal award date
Not reported
Contract end date
Not reported
UEI
Not reported
Solicitation number
Not reported
Topic code
Not reported

Research abstract

REAL-TIME FLUTTER PREDICTION INCLUDING CLOSE MODES CAN BE EFFECTIVELY ESTIMATED FROM TURBULENCE OR ON-BOARD EXCITATIONWITH AN EXTENDED KALMAN FILTER(EKF) APPROACH. THE THE PHYSICALLY BASED MODEL FORM ENABLES PREDICTION OF THE DAMPING RATE AS WELL AS DAMPING GIVING A TIME TO UNSTABILITYESTIMATE WITH IT'S VARIANCE. THE APPROACH IS RECURSIVE AND CAN OPERATE A SYNNCCHRON AND CAN OPERATE A SYNCHRONOUSLY TO DROP ATA OUTLINERS AND HENCE IS QUITE ROBUST. IT'S SPEED IS REASONABLE FOR ON-LINEAPPLICATION BUT ALSO CAN BE USED EFFECTIVELY AS AN OFF-LINE ANALYSIS TOOL FOR APPLICATION TO ANY MODEL TESTING SITUATION.

Technology keywords

Not reported

Agency intelligence

National Aeronautics and Space Administration

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