Handheld terminal, aircraft, airspace measuring method and control method of aircraft

Abstract

The invention provides a handheld terminal, an aircraft, an airspace measuring method and a control method of the aircraft, a flight system and a flight method of the flight system. The handheld terminal comprises: a measuring unit that measures position information of at least one target object in a peripheral space where the aircraft is located; a modeling unit that is used for modeling the peripheral space where the aircraft is located according to the position information of the at least one target object so as to generate modeling information; a control unit that generates control information based on at least the modeling information; and a communication unit that transmits the control information based on at least the modeling information to the aircraft.

Description

technical field [0001] The present disclosure relates to the field of aircraft, and in particular to a handheld terminal, an aircraft and its airspace measurement method, control method, and flight system and its flight method. Background technique [0002] The bionic flapping wing aircraft has a development history of more than 30 years. Usually, in order to realize the flight mode of the bionic flapping wing, the fuselage weight of this type of aircraft is required to be relatively light. For example, the toy products of the bionic flapping wing aircraft on the market weigh about 10 grams, basically no more than 15 grams. [0003] This may lead to technical difficulties such as low load capacity of the bionic flapping wing aircraft, few functions of the on-board control module, and poor autonomous flight capability. On the other hand, the current remote controllers suitable for this type of bionic flapping-wing aircraft are too simple in function, and generally only have...

AI Technical Summary

Problems solved by technology

[0003] This may lead to technical difficulties such as low load capacity of the bionic flapping wing aircraft, few functions of the on-board control module, and poor autonomous flight capability.

On the other hand, the current remote controllers suitable for this type of bionic flapping-wing aircraft are too simple in function, and generally only have four flight control modes: up, down, left, and right, and cannot give slightly more complicated control commands, so it cannot be realized. More complex flight modes such as autonomous flight, obstacle avoidance flight, follow-up flight, and homing

These factors hinder the commercial application of bionic flapping wing aircraft

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