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The three stage transfer process from GTO to GEO is realized by simulation and continuous small thrust. The thrust of the thruster is 0.8N, and the starting point of orbital maneuver is the apogee of GTO. GTO orbit RAAN
Date : 2025-06-16 Size : 44kb User : 大柚子

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PCA example code from image data
Date : 2025-06-16 Size : 10.32mb User : youdalj

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The least squares polynomial curve fitting, according to the given M point, does not require the curve to pass precisely these points, but rather the approximate curve of the curve y=f (x).
Date : 2025-06-16 Size : 3kb User : 氮气离子

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STAY HAPPY, STAY HEALTHY, GOOD LUCK
Date : 2025-06-16 Size : 888kb User : chintu12345

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eimdjoiebuaiekvmoreinvierjneroijcn
Date : 2025-06-16 Size : 33kb User : chintu12345

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svm_dataset for download
Date : 2025-06-16 Size : 1kb User : mavi

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svm regeression matlab
Date : 2025-06-16 Size : 171kb User : mavi

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Ideal Low-Pass Filter
Date : 2025-06-16 Size : 220kb User : ssennaa

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Amplitude Modulation
Date : 2025-06-16 Size : 163kb User : ssennaa

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Auto Correlation with matlab
Date : 2025-06-16 Size : 179kb User : ssennaa

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PSD of human voice with matlab
Date : 2025-06-16 Size : 164kb User : ssennaa

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The code is suitable for ofdm
Date : 2025-06-16 Size : 4kb User : mahmoodi
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