Ten-Koh is a 23.5 kg, low-cost satellite developed to conduct space environment effects research in low-Earth orbit (LEO). Ten-Koh was developed primarily by students of the Kyushu Institute of Technology (Kyutech) and launched on 29 October 2018 on-board HII-A rocket F40, as a piggyback payload of JAXA’s Greenhouse gas Observing Satellite (GOSAT-2). The satellite carries a double Langmuir probe, CMOS-based particle detectors and a Liulin spectrometer as main payloads. This paper reviews the design of the mission, specifies the exact hardware used, and outlines the implementation and operation phases of the project. This work is intended as a reference that other aspiring satellite developers may use to increase their chances of success. Such a reference is expected to be particularly useful to other university teams, which will likely face the same challenges as the Ten-Koh team at Kyutech. Various on-orbit failures of the satellite are also discussed here in order to help avoid them in future small spacecraft. Applicability of small satellites to conduct space-weather research is also illustrated on the Ten-Koh example, which carried out simultaneous measurements with JAXA’s ARASE satellite.
Automatic Digital Modulation Recognition (ADMR) is becoming an interesting problem with various civil and military applications. In this paper, anADMRalgorithm in Multi-Carrier Code Division Multiple Access (MC-CDMA) systems using Discrete Transforms (DTs) and Mel-FrequencyCepstral Coefficients (MFCCs)is proposed.Thisalgorithm usesvarious DT techniques such as the Discrete Wavelet Transform (DWT), Discrete Cosine Transform (DCT) and Discrete Sine Transform (DST) with MFCCs to extract features from the modulated signal and aSupport Vector Machine(SVM) to classify the modulation orders. Theproposed algorithm avoids over fitting and local optimal problems that appear in Artificial Neural Networks (ANNs). Simulation results shows the classifier is capable of recognizing the modulation scheme with high accuracy up to 90%-100% using DWT, DCT and DST for some modulation schemesover a wide Signal-to-Noise Ratio (SNR) range in the presence of Additive White Gaussian Noise (AWGN) and Rayleigh fading channel, particularly at a low Signal-to-Noise ratios (SNRs).
In each stage of any satellite design cycle, it is required to have test system that verifies the operational functions of each satellite subsystem and the integration operation among the satellite subsystems. Usually, these test systems consist of many hardware's and these hardware's are very complicated and occupied large space. The first Egyptian satellite, Egypt Sat-1, has a test center; a place where the satellite integration test sequences are carried out. This center consists of complicated hardware. In this paper a new trend, using LabView tool with National Instrument (NI) chassis, is used to build a satellite test center (STC) prototype that reduce the cost, complexity and occupied area of the STC. So the new trend tests the ability to replace the Egypt Sat-1 test center. The results of this paper shows that the quality of the new trend compared to the existed Egypt Sat-1 test center.
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