漫游者-背靠背CANSAT的设计与实现

Proceedings of 5th International Conference on Recent Advances in Space Technologies - RAST2011 Pub Date : 2011-06-09 DOI:10.1109/RAST.2011.5966952

M. Aydemir, M. Celebi, Serdar Ay, E. V. Vivas, Fredy Calle Bustinza, D. Phan

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引用次数: 10

摘要

在本研究中，设计并实现了一种具有返回目标能力的卫星。该设备是和歌山大学CLTP (CanSat领导力培训计划)项目的一部分。CanSat由最先进的MBED 32位微控制器控制。主要由压力传感器、超声波传感器、gps传感器和2.4 GHZ发射机组成。该任务计划分为两个阶段，由滑翔伞飞回目标，并在地面上用轮子漫游。这一过程将通过GoogleEarth软件在地面站进行监控。本文对系统的电子、硬件设计和控制算法进行了深入的讨论。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Design and implementation of a rover-back CANSAT

In this study, a CanSat with capability of returning back to target is designed amd implemented. The device is a part of project that has been implemented during the CLTP (CanSat Leadership Training Program) in Wakayama University. The CanSat is controlled by a state-of-the-art MBED 32-bit microcontroller. The main components are the pressure, ultrasonic, gps sensors and the 2.4 GHZ transmitter. The mission is planned for two stages which are flight back to the target by a paraglider and rovering on the ground on wheels. The process will be monitored on the ground station via the GoogleEarth software. The electronics&hardware design and the control algorithm is discussed in depth in this paper.

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Proceedings of 5th International Conference on Recent Advances in Space Technologies - RAST2011

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