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Novel Real-Time Flight Envelope Monitoring System

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX10CB57C
Agency Tracking Number: 080097
Amount: $600,000.00
Phase: Phase II
Program: STTR
Solicitation Topic Code: T2.01
Solicitation Number: N/A
Timeline
Solicitation Year: 2008
Award Year: 2010
Award Start Date (Proposal Award Date): 2010-08-13
Award End Date (Contract End Date): 2012-12-12
Small Business Information
420 N. Nash Street
El Segundo, CA 90245-2822
United States
DUNS: 121331057
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Michael Kerho
 Principal Investigator
 (310) 640-8781
 Mike.Kerho@RollingHillsResearch.com
Business Contact
 Brian Kramer
Title: Business Official
Phone: (310) 640-8781
Email: Brian.Kramer@RollingHillsResearch.com
Research Institution
 The Board of Trustees of the University of Illinois
 Walter Knorr
 
1901 South First Street, Suite A
Champaign, IL 61820
United States

 (217) 333-2187
 Domestic nonprofit research organization
Abstract

The proposed innovation is an aircraft flight envelope monitoring system that will provide real-time in-cockpit estimations of aircraft flight envelope boundaries. The adaptable system will provide information on current and predicted aircraft performance and controllability, alerting the pilot to any aerodynamic degradation of the aircraft control surfaces. This includes heavy rain, in-flight icing encounters, environmental contamination of surfaces, and structural damage such as bird strikes or battle damage. The real-time monitoring system measures the unsteady control surface hinge moment from all aircraft aerodynamic controls. Control surface hinge moments are sensitive to the aerodynamics of the section, including separation. These data are processed and information on the current and predicted future state of aircraft performance and control (including asymmetric cases) is made available to the pilot or flight management system. Phase I results have shown that the hinge moment sensor concept is a viable technology for the monitoring and prediction of airfoil stall. The hinge moment monitoring system was able to provide reliable stall warning and prediction across an incredibly wide range of simulated aerodynamic hazards. The proposed aircraft flight envelope monitoring system is an integral part of an overall integrated vehicle health management system.

* Information listed above is at the time of submission. *

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