Nonlinear adaptive trajectory tracking control for a stratospheric airship with parametric uncertainty

被引:0
作者
Liang Sun
Zewei Zheng
机构
[1] Beihang University,Seventh Research Division, Science and Technology on Aircraft Control Laboratory
来源
Nonlinear Dynamics | 2015年 / 82卷
关键词
Non-certainty equivalence principle; Adaptive control ; Trajectory tracking; Stratospheric airship;
D O I
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中图分类号
学科分类号
摘要
A nonlinear adaptive trajectory tracking control strategy is proposed for a fully actuated stratospheric airship subject to uncertain mass and inertia parameters. Based on the stratospheric airship trajectory tracking model, a non-certainty equivalence adaptive control approach is adopted to estimate the uncertain parameters since its excellently attractive property of the immersion and invariance manifold condition. The key idea involves a new filter construction for the regressor terms in the airship dynamics that enables the establishment of a stabilizing mechanism within the adaption process for uncertain parameters. It is proved that trajectory tracking errors asymptotically converge to zero within the Lyapunov framework. Numerical simulations are presented to demonstrate the performance of the proposed controller.
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页码:1419 / 1430
页数:11
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