A manual mode flight planning method, device and electronic equipment

Abstract

The application relates to a manual mode flight planning method, device and electronic equipment. The manual mode flight planning method comprises the following steps: building an offline wind resistance model, calculating a target speed under the current system, converting the target speed under the current system into a target speed under a local system and obtaining a target speed in a radial direction and a normal direction, calculating a planning acceleration feedforward, calculating a planning speed, calculating a planning position, and obtaining flight planning of a UAV under a manual mode. The device comprises a first acquisition module, a second acquisition module, a first conversion module, a first calculation module, a second calculation module, a third calculation module and a second conversion module. The device further comprises an electronic equipment. The manual mode flight planning method, device and electronic equipment can solve the problems that, under the existing manual mode, the input mapping and the guidance strategy present linear response, the start and stop are abrupt, inertia and damping transition are lacking, and the failure probability and flight risk are increased.

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