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International Journal of Aerospace System Science and Engineering最新文献

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Using photometric data to describe the behaviour of objects in geostationary orbit 利用光度数据来描述地球静止轨道上物体的行为
Pub Date : 1900-01-01 DOI: 10.1504/ijasse.2021.10039382
K. Sukhov, I. Motrunich, V. Yepishev, P. Sukhov
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引用次数: 0
Design and fabrication of 3D printed QuadDrone for altitude measurement 用于高度测量的3D打印四轴无人机的设计与制造
Pub Date : 1900-01-01 DOI: 10.1504/IJASSE.2021.10034731
B. Meenakshipriya, N. Raja, S. Faroshkhan, S. Matris
The main motivation towards the application of the proposed QuadDrone is precise altitude measurement. The QuadDrone is designed using SolidWorks and fabricated using 3D printing technology. The drone body is fabricated using poly lactic acid (PLA) material (black) and acrylonitrile butadiene styrene (ABS) material (white) is used to fabricate drone landing box. For this purpose, Ultimaker and CubePro 3D printers are used. The printed parts are tested for dimensional accuracy and surface roughness. The electronic components used for drone are flight control (KK2), electronic speed controllers (ESCs), transmitter and receiver (six channels), BLDC motors (2,280 KV), propellers (5045) and pressure sensor for altitude measurement (BMP180). The QuadDrone is assembled with 3D printed parts and electronics components. The difficulties encountered while developing the drone are assembly errors, sizing issues and weight balancing. The recent technologies like 3D printing, rapid prototyping and drone technology are used to develop the QuadDrone. The performance to measure the altitude of QuadDrone is tested in the open environment and it will act as a precision altimeter.
提出的QuadDrone应用的主要动机是精确的高度测量。QuadDrone使用SolidWorks设计,并使用3D打印技术制造。无人机机身采用聚乳酸(PLA)材料(黑色)制造,无人机着陆箱采用丙烯腈-丁二烯-苯乙烯(ABS)材料(白色)制造。为此,使用了Ultimaker和CubePro 3D打印机。对打印的零件进行尺寸精度和表面粗糙度测试。用于无人机的电子元件是飞行控制(KK2),电子速度控制器(esc),发射器和接收器(六通道),BLDC电机(2,280 KV),螺旋桨(5045)和用于高度测量的压力传感器(BMP180)。QuadDrone由3D打印部件和电子元件组装而成。在开发无人机时遇到的困难是装配错误,尺寸问题和重量平衡。最近的技术,如3D打印,快速原型和无人机技术被用于开发QuadDrone。在开放环境下测试了QuadDrone的高度测量性能,并将其作为精密高度计。
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引用次数: 3
Design and implementation of low-power low-cost quasi steady-state magnetoplasmadynamic propulsion using Ar-He and N2-He gas mixtures 利用Ar-He和N2-He混合气体设计和实现低功耗低成本准稳态磁等离子体动力推进
Pub Date : 1900-01-01 DOI: 10.1504/IJASSE.2021.10036799
C. Stoute
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引用次数: 0
Synthesising knowledge for lean product development process of a low noise jet engine 为低噪音喷气发动机精益产品开发过程提供综合知识
Pub Date : 1900-01-01 DOI: 10.1504/ijasse.2020.10031916
Z. Araci, A. Al-Ashaab, M. Tariq, Jan H. Braach
The product development process is one of the most challenging stages of a product life cycle due to several reasons. Having the right knowledge environment during the design process may eliminate the waste of cost and time. The aim of this paper is to demonstrate a case study where designers can investigate the conflicting parameters about a product and make their decisions based on an accurate knowledge environment that is created by trade-off curves. The product in consideration is a turbofan jet engine with a requirement of noise reduction during takeoff while keeping up with high quality standards.
由于几个原因,产品开发过程是产品生命周期中最具挑战性的阶段之一。在设计过程中拥有正确的知识环境可以消除成本和时间的浪费。本文的目的是展示一个案例研究,其中设计师可以调查关于产品的冲突参数,并根据权衡曲线创建的准确知识环境做出决策。该产品是要求在起飞时降低噪音并保持高质量标准的涡扇喷气发动机。
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引用次数: 0
Autonomous wildfire hotspot detection using a fixed wing UAV 利用固定翼无人机自主探测野火热点
Pub Date : 1900-01-01 DOI: 10.1504/IJASSE.2021.10036800
M. Wotton, H. Liu, D. Bohdanov, Zhongjie Lin
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引用次数: 0
Prospects of siting a spaceport in Africa 在非洲建立太空港的前景
Pub Date : 1900-01-01 DOI: 10.1504/IJASSE.2021.10036564
Sesugh Nongo, N. Ikpaya, Ikpaya O. Ikpaya
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引用次数: 0
Unique role of small satellites in empowering spacecraft formation flying missions 小卫星在增强航天器编队飞行任务中的独特作用
Pub Date : 1900-01-01 DOI: 10.1504/IJASSE.2021.10036565
P. Waswa
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引用次数: 0
The design concept of a small technological spacecraft 小型科技航天器的设计概念
Pub Date : 1900-01-01 DOI: 10.1504/ijasse.2023.10055071
A. Sedelnikov, Anastasiya Sergeevna Taneeva
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引用次数: 0
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International Journal of Aerospace System Science and Engineering
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