The theory of adaptive control of feedback linearizable systems is applied to designing the control of wing rock motion with the extension of the technique to include tracking. The adaptation law is designed to adjust the aerodynamic parameters in the model. Precise tracking and maximum performance can be achieved if sufficient rolling moment derivative because of lateral control components are available. Case studies and simulation are carried out to illustrate the results.
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Monahemi et al. (1996) studied this question.
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