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Calculation of aircraft sideslip angle
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Firstly, the quaternion is calculated by collecting three attitude angles of the sensor. The rotation matrix is formed by quaternion. The velocity in the geographical coordinate system is transformed into the body coordinate system by rotation matrix, and the sideslip angle of the current aircraft is calculated by trigonometric function
chengzhang1993 0 0
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Oscilloscope data acquisition
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The program is suitable for oscilloscope data acquisition, written with LabVIEW, suitable for Agilent oscilloscope (after the word, the program is suitable for oscilloscope data acquisition, written with LabVIEW, suitable for Agilent oscilloscope)
chengzhang1993 0 0
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