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Autonomous re-entry system technology demonstrator for sounding rockets: Development of an automated control system as recovery device for precise landing of sounding rockets

机译:探空火箭自主重入系统技术演示器:开发自动控制系统作为探空火箭精确着陆的恢复装置

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The Nimbus Project team, made of young engineers and university students, is developing an Autonomous Re-Entry System (ARES) based on a controlled paraglider. The target is to use the ARES to autonomously recover a reusable sounding rocket in a specific area dedicated for landing. The system is mainly divided in two parts: the paraglider wing with a traditional configuration of a ram-air parachute and the control box which houses the main control electronics. Furthermore, the sounding rocket is attached to the control box and a ground station receives telemetry or sends telecommands for both the rocket and the control box. In order to test the system in-flight independently from the launch of a rocket, a fully functional Technology Demonstrator has been developed. It is built from Commercial-Off-The-Shelf items and components and from custom composite parts. The mass of the wing is about 200g for a surface of 1.1m2 and the control box mass is 550g. The electronics communicates through telemetry and telecommands with a ground PC. Attitude and position sensors are used in the control loop and three modes of operation can be selected. The ARES has been already flight tested in direct control mode.
机译:由年轻工程师和大学生组成的Nimbus项目团队正在开发一种基于受控滑翔伞的自主重入系统(ARES)。目标是使用ARES在专用于着陆的特定区域中自主回收可重复使用的探空火箭。该系统主要分为两部分:滑翔伞机翼和传统的冲压空气降落伞配置,以及控制箱,其中装有主要的控制电子装置。此外,探空火箭安装在控制箱上,地面站接收遥测或发送火箭和控制箱的遥控指令。为了独立于火箭的发射而在飞行中对系统进行测试,已经开发了功能齐全的技术演示器。它由现成的商品和组件以及定制的复合零件构成。对于1.1平方米的飞机,机翼的质量约为200克,控制箱的质量为550克。电子设备通过遥测和遥控命令与地面PC进行通信。在控制回路中使用了姿态和位置传感器,并且可以选择三种操作模式。 ARES已经在直接控制模式下进行了飞行测试。

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