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Improving UAV Safety During Piloted Flight Phases by Keeping the Autonomous Controller in the Loop

机译:通过将自主控制器保持在回路中,在试飞阶段提高无人机安全性

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This paper presents the results of placing an H-infinity controller in the loop with the human pilot of a 33% scale Yak-54 UAV. An H-infinity controller is used because it is already present onboard the aircraft for use by its autonomous flight mode. The goal of the research was to improve the safety of the aircraft above that of the open loop aircraft. However, simulation of the control system with the H-infinity controller in the loop with pilot commands revealed surprising drawbacks. With the controller tuned to provide responses of similar magnitude and mode shape to that of the open loop aircraft, the system experienced a 0.2 to 0.3 second pure delay due to the presence of the H-infinity controller. Analysis shows this delay renders the control system response similar to that of an inebriated pilot. Changing the controller to reduce this delay resulted in exaggerated responses that could send the aircraft into unsafe flight regimes. In either case, the mismatch between pilot inputs and aircraft responses creates a risk of PIO. As a result, the Aerospace Department has decided not to implement this control scheme on a flight test aircraft due to the significant flight risks.
机译:本文介绍了将H-infinity控制器与33%比例的Yak-54无人机的飞行员放置在回路中的结果。使用H-infinity控制器是因为它已经存在于飞机上以供其自主飞行模式使用。研究的目的是提高飞机的安全性,使其高于开环飞机的安全性。但是,使用飞行员命令在回路中使用H-infinity控制器对控制系统进行仿真显示出令人惊讶的缺点。调整控制器以提供与开环飞机相似的幅度和模式形状的响应时,由于存在H-infinity控制器,系统经历了0.2到0.3秒的纯延迟。分析表明,这种延迟使控制系统的响应与飞行员失控的响应相似。更改控制器以减少这种延迟会导致响应过度,从而使飞机进入不安全的飞行状态。无论哪种情况,飞行员输入和飞机响应之间的不匹配都会产生PIO风险。结果,由于重大的飞行风险,航空航天部门决定不对飞行试验飞机实施该控制方案。

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