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A robust adaptive autopilot design for decomposed bank to turn missiles.

机译:一种强大的自适应自动驾驶仪设计,可用于分解银行以发射导弹。

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A decomposed robust adaptive controller design procedure is developed for 3-channel BTT missile systems. Three decomposed subsystems are constructed for highly nonlinear and coupled dynamic systems after parameter analysis is carried out. Appropriate adaptive optimal inner loop controllers are designed for accurate tracking performance to the reference command inputs of the respective subsystems.; For robustness of systems, decomposed outer loop structures are introduced to minimize system coupling and to reduce nonlinear effects of BTT missile dynamic systems. The overall outer loop robust controller is designed to accommodate parameter variations and uncertainties with referenced model systems. The robust outer loop controller is designed by constructing decomposed stabilizing controllers in the form of the Youla parameterization. The results can be readily generalized to N-channel systems. The design procedure is built upon the J-spectral factorization approach to H control. Instead of the centralized control, we employed decentralized controllers for reduced complexity in control implementations.; In this research, a new concept for system modeling and decomposition, which uses the rate of system dynamics or the sensitivity of system parameter. After exhaustive classification and investigations of system characteristics, we can categorize several subsystems from overall system dynamic models. Subsystems are characterized by system dynamics with similar rates of changes. Once we get relatively small sized and homogeneous parameter groups, it is easier to design respective controllers. Otherwise, difficult trade offs must be made on control objectives for different kinds of dynamic characteristics of the whole system. The new idea is applied to a typical BTT missile system. Simulations results demonstrate that decomposed controller design is satisfactory for the BTT missile autopilot systems with good robustness and dynamic performances.
机译:针对3通道BTT导弹系统,开发了一种分解的鲁棒自适应控制器设计程序。在进行参数分析之后,针对高度非线性和耦合的动态系统构建了三个分解子系统。设计适当的自适应最佳内环控制器,以对各个子系统的参考命令输入进行准确的跟踪。为了增强系统的鲁棒性,引入了可分解的外环结构以最小化系统耦合并减少BTT导弹动态系统的非线性影响。整体外环鲁棒控制器设计用于适应参考模型系统的参数变化和不确定性。通过构造Youla参数化形式的分解稳定控制器来设计鲁棒外环控制器。结果可以很容易地推广到N通道系统。该设计过程建立在J谱分解方法的H 控制上。代替集中控制,我们采用了分散控制器来降低控制实现的复杂性。在这项研究中,提出了一种用于系统建模和分解的新概念,该概念使用系统动态速率或系统参数的敏感性。经过详尽的分类和对系统特性的研究,我们可以从整体系统动态模型中对几个子系统进行分类。子系统的特点是系统动力学具有相似的变化率。一旦我们获得相对较小的大小和同质的参数组,就可以更轻松地设计相应的控制器。否则,必须针对整个系统的各种动态特性在控制目标上做出艰难的取舍。新的想法被应用于典型的BTT导弹系统。仿真结果表明,分解后的控制器设计对于具有良好鲁棒性和动态性能的BTT导弹自动驾驶系统是令人满意的。

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