Loss-of-Control Prediction of a Quadcopter Using Recurrent Neural Networks

被引:2
作者
Altena, Anique V. N. [1 ]
van Beers, Jasper J. [2 ]
de Visser, Coen C. [2 ]
机构
[1] Delft Univ Technol, Fac Aerosp Engn, Aircraft Noise & Climate Effects Sect, Kluyverweg 1, NL-2629 HS Delft, Netherlands
[2] Delft Univ Technol, Fac Aerosp Engn, Control & Simulat Sect, Kluyverweg 1, NL-2629 HS Delft, Netherlands
来源
JOURNAL OF AEROSPACE INFORMATION SYSTEMS | 2023年 / 20卷 / 10期
关键词
Quadcopter; Convolutional Neural Network; Flight Control Surfaces; Unmanned Aerial Vehicle; Aerodynamic Characteristics; Avionics Software; Onboard Sensors; Computing and Informatics; Aircraft Wing Design; Flight Testing; SAFE FLIGHT-ENVELOPE; AIRCRAFT LOSS; CONTROL PREVENTION; PROTECTION;
D O I
10.2514/1.I011231
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Loss of control (LOC) is a prevalent cause of drone crashes. Onboard prevention systems should be designed requiring low computing power, for which data-driven techniques provide a promising solution. This study proposes the use of recurrent neural networks (RNNs) for LOC prediction. Four architectures were trained in order to identify which RNN configuration is most suitable and if this model can predict LOC for changing aerodynamic characteristics, wind conditions, quadcopter types, and LOC events. One-hundred and seventy-two real-world LOC events were conducted using a 53 g Tiny Whoop, a 73 g URUAV UZ85, and a 265 g GEPRC CineGO quadcopter. For these flights, LOC was initiated by demanding an excessive yaw rate (2000 deg/s), which provokes an unrecoverable upset and subsequent crash. All RNNs were trained using only onboard sensor measurements. It was found that the commanded rotor values provided the clearest early warning signals for LOC because these values showed saturation before LOC. Moreover, all four architectures could correctly and reliably predict the impending LOC event 2 s before it actually occurred. Furthermore, to investigate generality of the methodology, the predictors were successfully applied to flight data in which the quadcopter mass, blade diameter, and blade count were varied.
引用
收藏
页码:648 / 659
页数:12
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