STANDARD OPTIMAL PILOT MODELS

机译：标准的最佳驾驶员模型

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An optimal control theoretic model of the human pilot is developed which is compatible with the most recent linear, multivariable, optimal control solutions. The model formulation matches that of existing H2/LQG models, yet can also be used to define a new H-infinity model. Comparisons are shown between existing models, measured data, and the new model formulation for position, velocity, and acceleration controlled elements.

机译：开发了与最新线性，多变量，最优控制解决方案兼容的人类飞行员的最优控制理论模型。该模型公式与现有的H2 / LQG模型相匹配，但也可以用于定义新的H-无限模型。显示了现有模型，测量数据和位置，速度和加速度控制元素的新模型公式之间的比较。

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《AIAA Guidance, Navigation and Control Conference Pt.2, Aug 1-3, 1994, Scottsdale, AZ》|1994年|p.750-756|共7页
会议地点 Scottsdale AZ(US)
作者
Mark R. Anderson;
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作者单位

Virginia Polytechnic Institute and State University Blacksburg, VA 24061;

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原文格式 PDF
正文语种 eng
中图分类航空;
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机译：标准最优试点型号
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机译：用最优和次优先导模型预测飞行员意见评级

STANDARD OPTIMAL PILOT MODELS

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