The invention discloses a flight parameter determination method and device, an aircraft and a computer readable storage medium, the method is applied to the aircraft, the aircraft comprises N rotor wings and N rotor wing motors, the N rotor wings and the N rotor wing motors are in one-to-one correspondence, N is an integer greater than 1, and the method comprises the following steps: obtaining a measured current air pressure height of the aircraft, determining the current rotating speed of the N rotor motors, determining the current barometric altitude error according to the current rotating speed of the N rotor motors, and determining the barometric altitude of the aircraft according to the current barometric altitude error and the current barometric altitude of the aircraft to obtain a first barometric altitude, and determining a first flight height and a first vertical speed of the aircraft according to the first air pressure height. In the embodiment of the invention, the measured barometric altitude is compensated by using the current barometric altitude error, so that the accuracy of the determined barometric altitude can be improved, and the accuracy of the determined flight altitude and vertical speed of the aircraft can be further improved.
本申请公开了一种飞行参数确定方法、装置、飞行器及计算机可读存储介质,该方法应用于飞行器,飞行器包括N个旋翼和N个旋翼电机,N个旋翼与N个旋翼电机一一对应,N为大于1的整数,该方法包括:获取测量的飞行器的当前气压高度,确定N个旋翼电机的当前转速,根据N个旋翼电机的当前转速确定当前气压高度误差,根据当前气压高度误差和飞行器的当前气压高度确定飞行器的气压高度得到第一气压高度,根据第一气压高度确定飞行器的第一飞行高度和第一垂向速度。本申请实施例中,由于使用当前气压高度误差对测量的气压高度进行了补偿,因此,可以提高确定的气压高度的准确性,进而可以提高确定的飞行器的飞行高度和垂向速度的准确性。
Flight parameter determination method and device, aircraft and computer readable storage medium
飞行参数确定方法、装置、飞行器及计算机可读存储介质
2024-03-26
Patent
Electronic Resource
Chinese
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