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Direct model reference adaptive control with application to damage mitigation of actively controlled structures.

机译:直接模型参考自适应控制,可应用于主动控制结构的减震。

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Structural damage is a potential hazard to every aerospace vehicle. Damage to an adaptive structure carries with it the additional hazard of a servo-elastic instability. To prevent an impact damage from causing a servo-elastic instability, the control system must either: be robust enough to tolerate the change in the plant; identify the change and switch to a more appropriate control law; or adaptively control the structure.; This research focuses on the latter approach. The adaptive theory Direct Model Reference Adaptive Control (DMRAC), developed by Wen and Balas, is the foundation for this research. The applicability of this approach with a piecewise constant plant is evaluated. Model matching conditions are derived for a general plant, and these conditions are evaluated for a second order plant to gain insight into the physical significance of these matching conditions. Additionally, criteria to ensure the strict positive real condition are developed for the second order example.; The theoretical foundations for using the DMRAC approach with a reduced order reference model are also presented. Of particular significance, is the use of the asymmetric Lyapunov matrix equation to provide sufficient conditions for the existence of ideal gains. These conditions determine whether or not a plant can be matched by a reduced order reference model.; Simulation results are presented for both a first order and a second order system. Based on the simulation results, DMRAC shows significant potential for maintaining control in the presence of damage, and for forcing the damaged plant to track a desired trajectory. Additionally, the frequency of the damaged plant was found to have a more significant effect on the response than does the damping ratio. Using the simulations as a guide, a designer should base the selection of the reference model on desirable transient behavior, and not be concerned with how the damaged structure will behave.
机译:结构损坏是每架航空航天飞机的潜在危害。自适应结构的损坏会带来伺服弹性不稳定的额外危险。为了防止冲击损坏引起伺服弹性不稳定,控制系统必须:足够坚固以承受工厂的变化;确定变更并改用更合适的控制法则;或自适应地控制结构。这项研究侧重于后一种方法。 Wen和Balas提出的自适应理论直接模型参考自适应控制(DMRAC)是这项研究的基础。评估了该方法在分段恒定工厂中的适用性。为一般工厂导出模型匹配条件,并为二阶工厂评估这些条件,以深入了解这些匹配条件的物理意义。另外,为二阶示例开发了确保严格的正真实条件的标准。还介绍了使用带有降阶参考模型的DMRAC方法的理论基础。特别重要的是,使用非对称Lyapunov矩阵方程为存在理想增益提供了充分的条件。这些条件决定了工厂是否可以通过降阶参考模型进行匹配。给出了针对一阶和二阶系统的仿真结果。基于仿真结果,DMRAC显示出在存在损坏时保持控制力和迫使受损工厂跟踪所需轨迹的巨大潜力。此外,发现受损设备的频率对响应的影响比阻尼比更为显着。使用模拟作为指导,设计人员应在参考模型的选择基于所需的瞬态行为的基础上,而不必关心受损结构的行为方式。

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