Numerical computation and approximations of H/sup infinity / optimal controllers for a 2-parameter distributed model of an unstable aircraft

D. Enns, H. Ozbay, A. Tannenbaum
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引用次数: 2

Abstract

The numerical computation of H/sup infinity / optimal controllers for an unstable aircraft model with a time delay is discussed. It is shown that the optimal H/sup infinity / controller for this infinite-dimensional model can be computed from a finite determinantal formula. The properties of the optimal controller are examined. For a particular choice of weights, it is shown with an example that the optimal controller is stable and continuous. Approximations of this controller and suboptimality of the controllers obtained from these approximations are shown.<>
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非稳定飞机2参数分布模型H/sup∞/最优控制器的数值计算与逼近
讨论了一类具有时滞的不稳定飞机模型的H/sup∞/最优控制器的数值计算。结果表明,该模型的最优H/sup∞/控制器可由有限行列式计算得到。研究了最优控制器的性质。对于特定的权值选择,通过实例证明了最优控制器是稳定连续的。给出了该控制器的近似和由这些近似得到的控制器的次优性。
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