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Fundamental Study on Adaptive Shock Response Control for Emergency Landing of UAVs and Its Experimental Investigation 无人机紧急降落自适应冲击响应控制的基础研究及实验研究
Q2 Engineering Pub Date : 2023-01-01 DOI: 10.1541/ieejjia.23004526
Pengcheng Li, Ryuki Sato, Masaki Hasegawa, Susumu Hara
Unmanned aerial vehicles (UAVs) are widely used in many fields, including agriculture and industry. Touchdown of a UAV without tipping over is a crucial but challenging issue owing to disturbances and uncertainties in the landing phase. In particular, when a breakdown occurs in a UAV system and the UAV free falls, sensors can be destroyed or the integrity of the UAV can be compromised. Therefore, developing an emergency landing system that can suppress rebound after free falling and preserve the integrity of UAVs is necessary. This paper proposes an adaptive shock response mechanism as a safe and robust emergency landing system for UAVs. A spring-damper system combined with a plastic deformation part serves as this emergency landing system to absorb and mitigate the impact during the landing phase to avoid tipping over of a UAV by reducing the rebound height. A release system that unlocks the plastic deformation part when the landing height is sufficiently high is proposed. Numerical simulations are conducted to evaluate the performance of the proposed emergency landing system, which is compared with those of two other mechanisms. The results reveal that the proposed method can deliver satisfactory rebound-reducing performance and high robustness against variations in the UAV weight and falling height. Additionally, the effectiveness of the proposed mechanism is experimentally validated using an equivalent model.
无人驾驶飞行器(uav)广泛应用于农业和工业等许多领域。由于着陆阶段的干扰和不确定性,无人机的无倾覆着陆是一个关键但具有挑战性的问题。特别是,当UAV系统发生故障并且UAV自由落体时,传感器可能被破坏或UAV的完整性可能受到损害。因此,开发一种能够抑制无人机自由落体后回弹并保持其完整性的应急着陆系统是十分必要的。本文提出了一种自适应冲击响应机制,作为一种安全鲁棒的无人机应急着陆系统。该紧急着陆系统采用弹簧-阻尼器系统与塑性变形部件相结合,通过降低弹跳高度来吸收和减轻着陆阶段的冲击,避免无人机倾覆。提出了一种当着陆高度足够高时将塑性变形部分解锁的释放系统。通过数值仿真对所提出的紧急着陆系统进行了性能评价,并与其他两种机构进行了比较。结果表明,该方法具有较好的减弹性能和较强的鲁棒性,能够抵抗无人机重量和下落高度的变化。此外,利用等效模型对所提出机制的有效性进行了实验验证。
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引用次数: 0
High-Performance Sensorless Force Control Using Superior Wideband and Periodicity-Cancellation Force Observer 高性能无传感器力控制-基于宽带和周期性对消力观测器
IF 1.7 Q2 Engineering Pub Date : 2023-01-01 DOI: 10.1541/ieejjia.22000390
Thao Tran Phuong, Kiyoshi Ohishi, Y. Yokokura
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引用次数: 1
Robust Velocity Control for Electromagnetic Friction Brake Based on Disturbance Observer 基于扰动观测器的电磁摩擦制动器鲁棒速度控制
IF 1.7 Q2 Engineering Pub Date : 2023-01-01 DOI: 10.1541/ieejjia.22004484
Masaki Takeuchi, S. Katsura
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引用次数: 1
Inhaler Motion Evaluation Via Weighted DP Matching 基于加权DP匹配的吸入器运动评价
IF 1.7 Q2 Engineering Pub Date : 2023-01-01 DOI: 10.1541/ieejjia.22004514
A. Hasegawa, T. Shimono, Shunya Takano, K. Masaki, Hideo Nakada, M. Nishie, Jun Hakamata
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引用次数: 0
Accurate Leakage Inductance Modeling Using an Artificial Neural Network Based on the Dowell Model 基于Dowell模型的人工神经网络漏感精确建模
IF 1.7 Q2 Engineering Pub Date : 2023-01-01 DOI: 10.1541/ieejjia.22007452
Yuhan Wu, K. Shigematsu, Yasumichi Omoto, Yoshihiro Ikushima, J. Imaoka, Masayoshi Yamamoto
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引用次数: 0
Modeling, Analysis, and Experimental Validation of Magnetic Geared Linear Motor 磁齿轮直线电机的建模、分析与实验验证
IF 1.7 Q2 Engineering Pub Date : 2023-01-01 DOI: 10.1541/ieejjia.22007992
N. Khuong, T. Shimono
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引用次数: 0
Reduced Order Modeling of Half-Wave Rectified Brushless Synchronous Motor for Model-Based Design 基于模型设计的半波整流无刷同步电机降阶建模
IF 1.7 Q2 Engineering Pub Date : 2023-01-01 DOI: 10.1541/ieejjia.22011214
T. Koga, T. Abe, Yoshitsugu Otomo, Masaki Yamamoto, M. Rosu
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引用次数: 0
Motion Generation Based on Contact State Estimation Using Two-stage Clustering 基于两阶段聚类的接触状态估计运动生成
IF 1.7 Q2 Engineering Pub Date : 2023-01-01 DOI: 10.1541/ieejjia.22012635
K. Takeuchi, S. Sakaino, T. Tsuji
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引用次数: 0
Design of a Thrust Controller for Propeller Driven Systems Operating at Multiple Wind Velocities and Propeller Angular Velocities 多风速和螺旋桨角速度下螺旋桨驱动系统推力控制器的设计
IF 1.7 Q2 Engineering Pub Date : 2023-01-01 DOI: 10.1541/ieejjia.23000763
Yusuke Tsuji, D. Yashiro, Yuki Kato, Shinichiro Bando, K. Yubai, S. Komada
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引用次数: 0
Evaluation of DC Excitation of External-Rotor-Segment-Type SRM for Power Generation 发电用外转子分段式SRM直流励磁评价
IF 1.7 Q2 Engineering Pub Date : 2023-01-01 DOI: 10.1541/ieejjia.22003267
S. Hirayama, S. Takagi
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引用次数: 1
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IEEJ Journal of Industry Applications
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