Kalman-Filter-Based Adaptive Control: flight testing on general aviation aircraft

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Authors
Rafi, Melvin
Steck, James E.
Watkins, John Michael
Advisors
Issue Date
2017-09
Type
Article
Keywords
Research Projects
Organizational Units
Journal Issue
Citation
Melvin Rafi, James E. Steck, and John Watkins. "Kalman-Filter-Based Adaptive Control: Flight Testing on General Aviation Aircraft", Journal of Guidance, Control, and Dynamics, Vol. 40, Special Issue on The Kalman Filter and Its Aerospace Applications (2017), pp. 2307-2315
Abstract

Sensor noise and turbulence effects have been prevalent issues in control system design. Although a control system may respond well to “clean” input signals and commands in simulation, this may not be the case when a controller is tasked to perform in a practical environment. A sensor measurement from the plant may be distorted with noise, or turbulence effects may alter controller behavior. Across various engineering disciplines, the notion of engineered resilience has received much attention in efforts to design safer and more reliable systems [1,2] capable of tolerating uncertainties and disturbances.

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Publisher
American Institute of Aeronautics and Astronautics, Inc.
Journal
Book Title
Series
Journal of Guidance, Control, and Dynamics;v.40:no.9
PubMed ID
DOI
ISSN
0731-5090
EISSN