首页> 外文会议>Conference on AIAA guidance, navigation, and control >Subscale Flight Testing for Aircraft Loss of Control: Accomplishments and Future Directions
【24h】

Subscale Flight Testing for Aircraft Loss of Control: Accomplishments and Future Directions

机译:用于飞机丧失控制的亚电缆飞行试验:成就和未来方向

获取原文

摘要

Subscale flight-testing provides a means to validate both dynamic models and mitigation technologies in the high-risk flight conditions associated with aircraft loss of control. The Airborne Subscale Transport Aircraft Research (AirSTAR) facility was designed to be a flexible and efficient research facility to address this type of flight-testing. Over the last several years (2009-2011) it has been used to perform 58 research flights with an unmanned, remotely-piloted, dynamically-scaled airplane. This paper will present an overview of the facility and its architecture and summarize the experimental data collected. All flights to date have been conducted within visual range of a safety observer. Current plans for the facility include expanding the test volume to altitudes and distances well beyond visual range. The architecture and instrumentation changes associated with this upgrade will also be presented.
机译:子电路飞行测试提供了一种验证动态模型和缓解技术,在与飞机失去控制相关的高风险飞行条件下进行动态模型和缓解技术。 Airborne Subscale运输机研究(Airstar)设施旨在成为一种灵活而有效的研究设施,以解决这种飞行测试。在过去的几年(2009-2011)中,它已被用来用一个无人驾驶,远程驾驶的动态缩放的飞机进行58个研究航班。本文将概述设施及其架构,并总结收集的实验数据。所有迄今的航班都已在安全观察者的视觉范围内进行。当前的设施计划包括将测试量扩展到高度,远距离视觉范围。还将呈现与此升级相关的架构和仪器更改。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

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