首页> 外文OA文献 >The NASA Dryden AAR Project: A Flight Test Approach to an Aerial Refueling System
【2h】

The NASA Dryden AAR Project: A Flight Test Approach to an Aerial Refueling System

机译:NASA Dryden AAR项目:空中加油系统的飞行测试方法

代理获取
本网站仅为用户提供外文OA文献查询和代理获取服务,本网站没有原文。下单后我们将采用程序或人工为您竭诚获取高质量的原文,但由于OA文献来源多样且变更频繁,仍可能出现获取不到、文献不完整或与标题不符等情况,如果获取不到我们将提供退款服务。请知悉。

摘要

The integration of uninhabited aerial vehicles (UAVs) into controlled airspace has generated a new era of autonomous technologies and challenges. Autonomous aerial refueling would enable UAVs to travel further distances and loiter for extended periods over time-critical targets. The NASA Dryden Flight Research Center recently has completed a flight research project directed at developing a dynamic hose and drogue system model to support the development of an automated aerial refueling system. A systematic dynamic model of the hose and drogue system would include the effects of various influences on the system, such as flight condition, hose and drogue type, tanker type and weight, receiver type, and tanker and receiver maneuvering. Using two NASA F/A-18 aircraft and a conventional hose and drogue aerial refueling store from the Navy, NASA has obtained flight research data that document the response of the hose and drogue system to these effects. Preliminary results, salient trends, and important lessons are presented.
机译:无人飞行器(UAV)与受控空域的融合产生了自动技术和挑战的新时代。自主的空中加油将使无人机能够在关键时间目标上行驶更长的距离和更长时间的游荡。 NASA Dryden飞行研究中心最近完成了一项飞行研究项目,旨在开发动态软管和锥套系统模型,以支持自动空中加油系统的开发。软管和锥套系统的系统动力学模型将包括对系统的各种影响,例如飞行条件,软管和锥套类型,油轮类型和重量,接收器类型以及油轮和接收器操纵。 NASA使用两架NASA F / A-18飞机和海军的传统软管和锥套空中加油站,获得了飞行研究数据,这些数据记录了软管和锥套系统对这些影响的响应。介绍了初步结果,显着趋势和重要教训。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
代理获取

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号