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  • 匿名
关注:1 2013-05-23 12:21

求翻译:本文针对无人机自主空中加油对接段的精确对接问题,在不考虑加油机尾涡干扰和加油锥套自由摆动及其对受油机影响的基础上,提出基于线性二次型最优调节器(LQR)的控制策略, 完成空中加油过程中对接段受油插头与加油锥套的精确对接。是什么意思?

待解决 悬赏分:1 - 离问题结束还有
本文针对无人机自主空中加油对接段的精确对接问题,在不考虑加油机尾涡干扰和加油锥套自由摆动及其对受油机影响的基础上,提出基于线性二次型最优调节器(LQR)的控制策略, 完成空中加油过程中对接段受油插头与加油锥套的精确对接。
问题补充:

  • 匿名
2013-05-23 12:21:38
Accurate docking problem for the UAV aerial refueling docking segment without considering the tanker trailing vortex interference and refueling drogue swing freely and its impact on oil machine based on proposed based on linear quadratic optimal regulator (lqr) control strategy, complete accurate do
  • 匿名
2013-05-23 12:23:18
This document is not the autonomous aerial refueling tanker for the paragraph to the precise question, fill in on the tail does not take into account the interference and fill cone free swing and its impact on the oil-based on the 2, based on linear time-optimal regulator (LQR) control strategy to c
  • 匿名
2013-05-23 12:24:58
This article in view of the unmanned aerial vehicle independent air refueling docking section precise docking question, in did not consider the accelerator trailing vortex disturbance and the basket free oscillation and in the foundation which affects to the receiver, proposed based on the linear tw
  • 匿名
2013-05-23 12:26:38
This paper focuses on unmanned autonomous aerial refueling and docking the exact pairing problems, without taking into account the tanker wake interference and gas sleeve swing freely and on the basis of the impact on the customer, based on linear quadratic optimal regulator (LQR) control strategy,
  • 匿名
2013-05-23 12:28:18
正在翻译,请等待...
 
 
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