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The Stability of an Aircraft under AutomaticnThrottle Control and the Cross-Coupling Effects with Elevator Control

机译：自动油门控制下飞机的稳定性及电梯控制的交叉耦合效应

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The stability of an aircraft with automatic throttle and elevator controls has been investigated theoretically using an analogue computer. Throttle application proportional to change in airspeed, incidence, or rate of pitch may provide damping of the long-period motion, but speed is shown to be the most suitable variable.nThe control of an aircraft having negative static margin is considered and shown to require either the addition of an integral control on the throttle or a combination of throttle and elevator controls.nWhere it is required to control height by means of the elevator, some aircraft flying under certain conditions can only be adequately stabilised by means of an automatic throttle control.

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D. E. Fry; M. R. Watts;
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年度 1963
页码 1-25
总页数 25
原文格式 PDF
正文语种 eng
中图分类工业技术;
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The Stability of an Aircraft under AutomaticnThrottle Control and the Cross-Coupling Effects with Elevator Control

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