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Integrated Resilient Aircraft Control Project
The Integrated Resilient Aircraft Control (IRAC) Project will conduct
research to advance the state of aircraft flight control to provide
onboard control resilience for ensuring safe flight in the presence of
unforeseen, adverse conditions. One focus examines state-of-the-art of
adaptive controls as a design option to provide enhanced stability and
maneuverability margins for safe landing. While many of its studies
focus on current and next generation transport aircraft, the results
will also have applications for other aircraft types, and to the
military and space sectors. The focus of the IRAC project research will
be to develop a set of validated multidisciplinary integrated aircraft
control design tools and techniques for enabling safe flight in the
presence of adverse conditions such as structural damage, control
surface failures, icing, or aerodynamic upsets. As such, carefully
integrated math models are required to model the interactions between
control inputs, trajectory planning and guidance, and the aircraft
structures and propulsion systems.
Details of the dynamics involved in an aircraft loss of control
situation are required to better understand how a system can best regain
control without further exacerbating the situation. Enhancements to
engine modeling for situations requiring improved engine response during
full or partial loss of flight control will also be developed.
Successful transition of this foundational research into the national
airspace system depends greatly on the ability to verify and validate
the novel control and guidance technologies, especially those based on
adaptive control. Verification and validation of these technologies will
be performed through a combination of analyses, simulation, wind tunnel
and flight testing using model-scale and full-scale (manned) test
vehicles. The IRAC Project will utilize selected proposals under the NRA
to leverage in-house fundamental research with academic institutions,
non-profit organizations, and industry partners performing fundamental
research to address knowledge and technology gaps.
The following are ROA-2007 NRA awards for the IRAC Project, with the most recent listed first.

| PI Last Name |
Title |
Organization |
State |
Award Date |
Year 1 Amount |
| Ackroyd |
Fast Response Engine Controller - Mission Adaptive Engine Controller |
Pratt & Whitney |
CT |
01/24/2007 |
$425,555 |
| Lavretsky |
Robust Composite Adaptive Control for Piloted Aircraft |
Boeing |
CA |
12/21/2007 |
$329,978 |
| Urnes |
Dynamic Flight Envelope Assessment and Prediction |
Boeing |
MO |
12/21/2007 |
$468,622 |
| Glavaski |
Verifiable Adaptive Control: Analysis and Design |
Honeywell |
MN |
12/21/2007 |
$302,000 |
| Merrill |
Fast Response Engine Controller Design |
Scientific Monitoring, Inc |
AZ |
12/19/2007 |
$204,000 |
| Perhinschi |
Integrated System for Immunity-Based Failure Detection, Identification, and Evaluation |
West Virginia University |
WV |
12/18/2007 |
$60,000 |
| Al-Ali |
Experimental validation of metrics-driven enhanced-safety (ME) adaptive control |
Carnegie Mellon University - West Coast Campus |
PA |
12/11/2007 |
$350,000 |
| Johnson |
Fight Validation of Metrics-Based Adaptive Control Methods |
Georgia Institute of Technology |
GA |
12/11/2007 |
$274,999 |
| Hovakimyan |
Adaptive Control with a priori Guaranteed Performance Bounds and Robustness/Stability Margins |
Virginia Polytechnic Institute and State Univ. |
VA |
12/11/2007 |
$233,017 |
| Tiwari |
Using symbolic constraint solving techniques for analyzing stability properties of adaptive control systems |
SRI International |
CA |
12/10/2007 |
$225,000 |
| Balakrishnan |
Adaptive Control with Stability Guarantee |
University of Missouri |
MO |
12/05/2007 |
$92,000 |
| Ingraffea |
Computational Methods in Physics-Based Modeling of Damaged Flight Structures |
Cornell University |
NY |
11/30/2007 |
$100,000 |
| Calise |
Development of LMI Analysis Tools for Learning Algorithms |
Georgia Institute of Technology |
GA |
11/30/2007 |
$288,000 |
| Tsiotras |
Advanced Methods for Intelligent Flight Guidance and Planning in Support of Pilot Decision Making |
Georgia Institute of Technology |
GA |
11/30/2007 |
$229,000 |
| Crespo |
An Adaptive Control Technology for Safe High-Performance Aircraft (ACTS) |
National Institute of Aerospace |
VA |
11/30/2007 |
$300,000 |
| Shin |
Fault Diagnosis and Prognosis and Reliable Flight Envelope Assessment |
National Institute of Aerospace |
VA |
11/30/2007 |
$298,000 |
| Rushby |
Multi-legged safety cases for adaptive systems supported by formal methods and mechanized analysis |
SRI International |
CA |
11/30/2007 |
$225,000 |
| Sarigul-Klijn |
Dynamically Constrained Adaptive Flight Path Planning Using Predictive Algorithms |
University of California Davis |
CA |
11/30/2007 |
$197,000 |
| Atkins |
A Damage-Resilient Flight Planning and Guidance System for Safe, Collaborative Emergency Management |
University of Michigan |
MI |
11/30/2007 |
$249,000 |
| Balas |
Analytical Validation Tools for Safety Critical Systems |
University of Minnesota |
MN |
11/30/2007 |
$300,000 |
| Hovakimyan |
Flight Validation of Metrics Driven Adaptive Control |
Virginia Polytechnic Institute and State Univ. |
VA |
11/30/2007 |
$306,400 |
| Tao |
Adaptive Control Techniques for Systems under Structural Uncertainties with Aircraft Control Applications |
University of Virginia |
VA |
11/29/2007 |
$100,000 |
| Patil |
In-flight load constraint estimation and residual life prediction for aircraft with discrete source damage |
Virginia Polytechnic Institute and State Univ. |
VA |
11/28/2007 |
$177,000 |
| Bernstein |
Minimal Modeling Direct Digital Adaptive Flight Control |
University of Michigan |
MI |
11/27/2007 |
$225,821 |

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+ Integrated Vehicle Health Management Project
+ Aircraft Aging and Durability Project
+ Integrated Intelligent Flight Deck Project
+ Integrated Resilient Aircraft Control Project
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