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Design of Fully Automatic Drone Parachute System with Temperature Compensation Mechanism for Civilian and Military Applications

机译:平民温度补偿机制全自动无人机降落伞系统设计

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摘要

Application of Unmanned Aerial Vehicles (a.k.a. drones) is becoming more popular and their safety is becoming a serious concern. Due to high cost of top-end drones and requirements for secure landing, development of reliable drone recovery systems is a hot topic now. In this paper, we describe the development of a parachute system with fall detection based on accelerometer-gyroscope MPU – 6050 and fall detection algorithm based on the Kalman filter to reduce acceleration errors while drone is flying. We developed the compensation algorithm for temperature-related accelerometer errors. The parachute system tests were performed from a small height on a soft surface. Later, the system was tested under real-world conditions. The system functioned effectively, resulting in parachute activation times of less than 0.5s. We also discuss the civilian and military applications of the developed recovery system in harsh (high temperature) environment.
机译:无人驾驶飞行器(A.K.A.Verones)的应用变得越来越受欢迎,其安全正处于严重关注。由于顶端无人机的高成本和安全着陆要求,可靠的无人机恢复系统的开发现在是一个热门话题。在本文中,我们描述了基于加速度计 - 陀螺MPU-6050和基于卡尔曼滤波器的落下检测算法的降落伞系统的开发,以减少无人机飞行的加速误差。我们开发了用于温度相关的加速度计误差的补偿算法。降落伞系统测试从软表面上的小高度进行。后来,该系统在现实世界的条件下进行了测试。系统有效地运行,导致降落伞激活时间小于0.5s。我们还讨论了苛刻(高温)环境中发达的恢复系统的民用和军事应用。

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