首页> 外文OA文献 >Simulation to Flight Test for a UAV Controls Testbed
【2h】

Simulation to Flight Test for a UAV Controls Testbed

机译:无人机控制测试台的飞行测试仿真

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 NASA Flying Controls Testbed (FLiC) is a relatively small and inexpensive unmanned aerial vehicle developed specifically to test highly experimental flight control approaches. The most recent version of the FLiC is configured with 16 independent aileron segments, supports the implementation of C-coded experimental controllers, and is capable of fully autonomous flight from takeoff roll to landing, including flight test maneuvers. The test vehicle is basically a modified Army target drone, AN/FQM-117B, developed as part of a collaboration between the Aviation Applied Technology Directorate (AATD) at Fort Eustis, Virginia and NASA Langley Research Center. Several vehicles have been constructed and collectively have flown over 600 successful test flights, including a fully autonomous demonstration at the Association of Unmanned Vehicle Systems International (AUVSI) UAV Demo 2005. Simulations based on wind tunnel data are being used to further develop advanced controllers for implementation and flight test.
机译:NASA飞行控制试验台(FLiC)是一种相对较小且价格便宜的无人机,专为测试高度实验性的飞行控制方法而开发。 FLiC的最新版本配置有16个独立的副翼段,支持C编码的实验控制器的实施,并且能够从起飞滚轴到着陆的完全自主飞行,包括飞行测试演习。该测试车基本上是经过改装的陆军目标无人机,AN / FQM-117B,是弗吉尼亚州Fort Eustis航空应用技术局(AATD)与美国宇航局Langley研究中心合作开发的一部分。已制造出数种车辆,并成功进行了600多次成功的试飞,其中包括在国际无人驾驶系统协会(AUVSI)UAV Demo 2005上进行的完全自主演示。基于风洞数据的仿真正被用于进一步开发用于实施和飞行测试。

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