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A Hazard Analysis Based Approach to Improve the Landing Safety of a Blended-wing-body Remotely Piloted Vehicle

机译:基于危害分析的混合机翼远程驾驶飞行器着陆安全改进方法

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The BUAA-BWB remotely piloted vehicle (RPV) designed by our research team encountered an unexpected landing safety problem in flight experiments.It has obviously affected further research project for Blended-wing-body (BWB) aircraft configuration characteristics.Searching for a safety improvement is an urgent requirement in the development work of the RPV.Combining with vehicle characteristics, a new systemic method called System-Theoretic Process Analysis (STPA) has been imported to apply on the RPV flight experiment hazard analysis.An uncontrolled system behavior “path sagging phenomenon” is identified by implementing a 3 degree of freedom simulation based on wind tunnel experiment data and establishing landing safety system dynamics archetype, then a derived safety improvement requirement emerges. To obtain higher safety design effectiveness and considering safety design precedence, a new longitudinal control surface “belly-flap” is used to eliminate hazards in landing.Finally, Flight experiments show that the hazardous factor has been correctly identified and the landing safety has been efficiently improved.
机译:我们的研究团队设计的BUAA-BWB遥控飞行器(RPV)在飞行实验中遇到了意外的着陆安全问题,显然影响了混合翼体(BWB)飞机配置特性的进一步研究项目。 RPV的研发工作迫在眉睫。结合车辆特性,引入了一种新的系统方法,称为系统理论过程分析(STPA),用于RPV飞行实验危险性分析。通过基于风洞实验数据进行三自由度仿真并建立起降安全系统动力学原型来识别“现象”,然后得出了对安全性改进的要求。为了获得更高的安全设计效果并考虑安全设计的优先顺序,使用了新型纵向控制面“腹部襟翼”来消除着陆中的危险。最后,飞行实验表明已正确识别了危险因素并且有效地着陆了安全改善。

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