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Self-organizing radial basis function networks for adaptive flight control and aircraft engine state estimation.

机译:自组织径向基函数网络,用于自适应飞行控制和飞机发动机状态估计。

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摘要

The performance of nonlinear control algorithms such as feedback linearization and dynamic inversion is heavily dependent on the fidelity of the dynamic model being inverted. Incomplete or incorrect knowledge of the dynamics results in reduced performance and may lead to instability. Augmenting the baseline controller with approximators which utilize a parametrization structure that is adapted online reduces the effect of this error between the design model and actual dynamics. However, currently existing parameterizations employ a fixed set of basis functions that do not guarantee arbitrary tracking error performance. To address this problem, we develop a self-organizing parametrization structure that is proven to be stable and can guarantee arbitrary tracking error performance. The training algorithm to grow the network and adapt the parameters is derived from Lyapunov theory. In addition to growing the network of basis functions, a pruning strategy is incorporated to keep the size of the network as small as possible. This algorithm is implemented on a high performance flight vehicle such as F-15 military aircraft. The baseline dynamic inversion controller is augmented with a Self-Organizing Radial Basis Function Network (SORBFN) to minimize the effect of the inversion error which may occur due to imperfect modeling, approximate inversion or sudden changes in aircraft dynamics. The dynamic inversion controller is simulated for different situations including control surface failures, modeling errors and external disturbances with and without the adaptive network. A performance measure of maximum tracking error is specified for both the controllers a priori. Excellent tracking error minimization to a pre-specified level using the adaptive approximation based controller was achieved while the baseline dynamic inversion controller failed to meet this performance specification. The performance of the SORBFN based controller is also compared to a fixed RBF network based adaptive controller. While the fixed RBF network based controller which is tuned to compensate for control surface failures fails to achieve the same performance under modeling uncertainty and disturbances, the SORBFN is able to achieve good tracking convergence under all error conditions.
机译:非线性控制算法(如反馈线性化和动态反演)的性能在很大程度上取决于动态模型的逼真度。对动力学的不完全或不正确的了解会导致性能降低,并可能导致不稳定。使用近似器增强基线控制器,该近似器利用在线适应的参数化结构,可以减少设计模型与实际动力学之间的此误差。但是,当前现有的参数化采用一组固定的基础函数,这些基础函数不能保证任意跟踪误差性能。为了解决这个问题,我们开发了一种自组织的参数化结构,该结构被证明是稳定的并且可以保证任意跟踪误差性能。 Lyapunov理论推导了用于增长网络和调整参数的训练算法。除了扩展基本功能网络外,还采用了修剪策略以使网络规模尽可能小。该算法在高性能飞行器(例如F-15军用飞机)上实现。基线动态反演控制器增加了自组织径向基函数网络(SORBFN),以最大程度地减少由于建模不完善,近似反演或飞机动力学突然变化而可能引起的反演误差的影响。动态逆变器控制器针对不同情况进行了仿真,包括控制面故障,建模误差和有无自适应网络的外部干扰。先验地为两个控制器指定了最大跟踪误差的性能度量。当基线动态反演控制器不满足此性能规格时,使用基于自适应逼近的控制器就可以将跟踪误差最小化到预定水平。还将基于SORBFN的控制器的性能与基于固定RBF网络的自适应控制器进行了比较。虽然基于RBF网络的固定式控制器经过调整以补偿控制面故障,但在建模不确定性和扰动下无法达到相同的性能,而SORBFN能够在所有误差条件下实现良好的跟踪收敛性。

著录项

  • 作者

    Shankar, Praveen.;

  • 作者单位

    The Ohio State University.;

  • 授予单位 The Ohio State University.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2007
  • 页码 174 p.
  • 总页数 174
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

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