NASA NTRS · 19790010456
Aircraft adaptive learning control
Abstract
The optimal control theory of stochastic linear systems is discussed in terms of the advantages of distributed-control systems, and the control of randomly-sampled systems. An optimal solution to longitudinal control is derived and applied to the F-8 DFBW aircraft. A randomly-sampled linear process model with additive process and noise is developed.
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Lee, P. S. T., Vanlandingham, H. F.. 1979-01-01. Aircraft adaptive learning control. https://ntrs.nasa.gov/citations/19790010456
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