Integrated Resilient Aircraft Control Project Full Scale Flight Validation
- Bosworth, John T.
- August 09, 2009.
- Physical Description:
- 1 electronic document
- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
- Objective: Provide validation of adaptive control law concepts through full scale flight evaluation. Technical Approach: a) Engage failure mode - destabilizing or frozen surface. b) Perform formation flight and air-to-air tracking tasks. Evaluate adaptive algorithm: a) Stability metrics. b) Model following metrics. Full scale flight testing provides an ability to validate different adaptive flight control approaches. Full scale flight testing adds credence to NASA's research efforts. A sustained research effort is required to remove the road blocks and provide adaptive control as a viable design solution for increased aircraft resilience.
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 20090034937., DFRC-1045., and NESC GN&C Face-to-face Meeting; 20090809; Chicago, IL; United States.
- No Copyright.
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