AIAA Guidance, Navigation, and Control Conference 2009
DOI: 10.2514/6.2009-5967
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A Loop Recovery Method for Adaptive Control

Abstract: This paper presents a new modification term for use in adaptive control to improve an already existing design. By employing this term in a conventional adaptive law, the loop transfer properties of a reference model associated with a non-adaptive control design can be preserved. Consequently, this term increases the level of confidence of adaptive flight control systems for purposes of increased flight safety. The results are illustrated on an unmanned combat aerial vehicle dynamic model.

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Cited by 50 publications
(42 citation statements)
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“…(49). Recently an adaptive loop recovery (ALR) modification term [25] was proposed with the objective of recovering the loop transfer properties of a chosen reference system. ALR modification can be introduced by letting St x xt T x xt, where x xt dxt=dxt 2 R sn and in this case s 1.…”
Section: Modifications To Derivative-free Adaptive Controlmentioning
confidence: 99%
“…(49). Recently an adaptive loop recovery (ALR) modification term [25] was proposed with the objective of recovering the loop transfer properties of a chosen reference system. ALR modification can be introduced by letting St x xt T x xt, where x xt dxt=dxt 2 R sn and in this case s 1.…”
Section: Modifications To Derivative-free Adaptive Controlmentioning
confidence: 99%
“…While the aspect of stabilization and command following can be dealt with in a nonlinear setting by employing Lyapunov stability analysis, issues related to margins can be addressed using the adaptive loop recovery (ALR) modification term proposed in Ref. 5. By employing ALR modification, the loop transfer properties of a reference system associated with a nominal control design are preserved in an adaptive system.…”
Section: Introductionmentioning
confidence: 99%
“…8 Generally, the standard MRAC has to be modified to improve robustness using the well-known σ -modification 5 and e-modification 9 or the recently developed optimal control modification 10 and adaptive loop recovery. 11 The aircraft responses due to a 60-ms time delay for the least-squares gradient method, RLS with η = 0.2, and neural network MRAC are illustrated in Figs. 14, 15, and 16.…”
Section: Flight Control Applicationmentioning
confidence: 99%