Take-off and landing platform for aircraft

Abstract

The invention provides a take-off and landing platform for assisting an aircraft to take off and land in a bumpy environment. The take-off and landing platform comprises a fixing plate and an attitude adjustment seat, wherein the fixing plate is used as a platform where the aircraft takes off and lands, and is used for fixing the aircraft before the aircraft takes off; the attitude adjustment seat is mounted on the lower side of the fixing plate and is used for stabilizing a space attitude of the fixing plate; and the attitude adjustment seat is at least provided with two degrees of freedom capable of rotating around the X axis and the Y axis. The multi-axis aircraft is fixed on the fixing plate before taking off, and the attitude adjustment seat dynamically stabilizes the attitude of the aircraft, so that the aircraft can be prevented from swinging back and forth, and good take-off conditions are supplied to taking off; and the stable fixing plate can supply a good landing environment to the multi-axis aircraft.

Description

technical field [0001] The invention relates to a take-off and landing platform of an aircraft, in particular to a take-off and landing platform of a multi-axis aircraft. Background technique [0002] A multicopter usually includes a fuselage, an arm, a flight control device, a power supply, an ESC, a motor, a rotor, and functional sensors. [0003] Electric helicopters usually also include empennage and tail-locking gyroscopes, control devices for controlling the periodic pitch and collective pitch of the rotor pitch, and the control devices include steering gears, swash plates, connecting rods and other components. [0004] Neither multicopters nor electric helicopters are suitable for taking off in a windy environment. At present, quadcopters can fly in winds below level 5; hexacopters can barely fly in winds of levels 6 to 7. The wind speed of category 5 wind is between 8 and 10.7 meters per second, the wind speed of category 6 wind is between 10.8 and 13.8 meters per ...

AI Technical Summary

Problems solved by technology

Obviously, the takeoff of the drone depends on the weather conditions, and it still cannot take off in a windy environment

This system can only solve the problem of UAV take-off in good weather environment. In the environment of strong wind and waves, the problem of UAV take-off and landing is still not solved.

In addition, the plate electromagnet and the electromagnet drive module connected to it are fixed on the ship, and the magnetic plate is fixed on the tripod of the drone. Due to the large span of the tripod of the drone, a large support is required Therefore, the area of ​​the flat electromagnet will be very large, not only the weight is heavy, the manufacturing cost is high, but also requires more power to maintain the fixation of the drone, which is poor in practicability

When the take-off and landing platform is set on the land driving device, the undulations of the road surface will cause the driving device and the landing platform to be bumpy, which is not conducive to the take-off and landing of the multi-axis aircraft

[0006] Existing multi-axis aircraft basically only adjust the flight attitude by changing the rotor speed. Translational flight needs to tilt the fuselage, thus increasing the windward area of ​​the fuselage, resulting in an increase in flight resistance, making the multi-axis aircraft slow in response and poor in maneuverability , the frequent acceleration and deceleration of the motor causes a large loss of kinetic energy, large heat loss of the motor, and low efficiency

Under the action of high-speed airflow, it is difficult to take off and land safely

Before taking off on the landing platform impacted by the high-speed airflow, the multi-axis aircraft has no protection measures, not only is it easy to be blown off by the high-speed airflow, but also cannot achieve safe and stable mobile take-off and landing

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