首页> 外文会议>Congress of the International Council of the Aeronautical Sciences >EXPERIMENT ON THE APPLICATION OF A CUBE TYPE GYROSCOPE-FREE INERTIAL MEASUREMENT UNIT ON LAPANS RUM PAYLOAD-TEST ROCKETS
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EXPERIMENT ON THE APPLICATION OF A CUBE TYPE GYROSCOPE-FREE INERTIAL MEASUREMENT UNIT ON LAPANS RUM PAYLOAD-TEST ROCKETS

机译:立方体型陀螺惯性测量装置在Lapans Rum有效载荷试火箭的应用实验

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This paper discuss the application of a Gyroscope Free Inertial Measurement Unit (GF-IMU) for rocket. A GF-IMU is an inertial measurement unit that uses only sets of accelerometers to compute both translation and rotational of a vehicle, which in this case was a rocket. The elimination of gyroscope caused the system to be much cheaper (low-cost), compared to conventional inertial measurement unit. A cube type GF-IMU was used as a case study. The system were implanted in a payload test rocket (Roket Uji Muatan, RUM). The rocket was launch in August 2009 as part of student payload rocket competitions held by Indonesian National Institute of Aeronautics and Astronautics (Lembaga Penerbangan dan Antariksa Nasional, LAPAN). The GF-IMU data were transmitted during flight and recorded on the ground station. Analysis were conducted to obtain the rocket translational and rotational accelerations by processing the data. The experience on manufacturing, transmitting, recording and processing data from GF-IMU on rocket application were described in the end his paper.
机译:本文讨论了陀螺免疫惯性测量单元(GF-IMU)对火箭的应用。 GF-IMU是一种惯性测量单元,仅使用一组加速度计来计算车辆的平移和旋转,在这种情况下是火箭。与传统的惯性测量单元相比,消除陀螺仪使系统更便宜(低成本)。使用立方体类型GF-IMU作为案例研究。该系统植入有效载荷测试火箭(Roket Uji Muatan,Rum)。该火箭于2009年8月推出,作为由印度尼西亚国家航空航天研究所(Lembaga Penerbangan Dan Antariksa Nasional,Lapan)持有的学生有效载火箭比赛的一部分。 GF-IMU数据在飞行期间传输并在地面站上录制。进行分析以通过处理数据来获得火箭平移和旋转加速度。最后描述了来自GF-IMU在火箭应用中的制造,传输,记录和处理数据的经验。

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