The invention discloses a dynamic balancing method and device for integrated flight and a computer readable storage medium, and the method comprises the steps: obtaining a current unbalance type if a first balance state of a first aircraft is monitored to be an unbalance state, selecting a second aircraft and a third aircraft of which the second balance state and the third balance state are non-unbalanced states; if the unbalance type is left-right unbalance, the selected second aircraft and the selected third aircraft are connected to the left side and the right side of the first aircraft respectively, and if the unbalance type is front-back unbalance, the selected second aircraft and the selected third aircraft are connected to the front end and the rear end of the first aircraft respectively; therefore, the integrated aircraft is in a non-unbalance state. According to the invention, a dynamic balancing scheme based on dynamic integrated flight of a plurality of aircrafts is realized, and the problems of imbalance of the fixed-wing aircrafts caused by temporary order change or temporary cargo adjustment and poor timeliness of manual adjustment are effectively solved.
本发明公开了一种合体飞行的动态配平方法、设备及计算机可读存储介质,其中,该方法包括:若监测到第一航空器的第一平衡状态为失衡状态,则获取当前的失衡类型,并选定第二平衡状态和第三平衡状态均为非失衡状态的第二航空器和第三航空器;若所述失衡类型为左右失衡,则将选定的所述第二航空器和所述第三航空器分别连接于所述第一航空器的左右两侧,若所述失衡类型为前后失衡,则将选定的所述第二航空器和所述第三航空器分别连接于所述第一航空器的前后两端,以使合体的航空器为非失衡状态。本发明实现了一种基于多个航空器动态合体飞行的动态配平方案,有效地解决了因订单临时变更或货物临时调整所造成的固定翼航空器失衡、且人工调整时效性较差的问题。
Dynamic balancing method and device for integrated flight and computer readable storage medium
一种合体飞行的动态配平方法、设备及计算机可读存储介质
2023-08-18
Patent
Electronic Resource
Chinese
IPC: | B64U |
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