System and method for flight stability control of unmanned aerial vehicle

Abstract

The invention discloses a UAV flight stability control system and method. The control system includes a base, the top of the base is provided with a mounting groove, and slide rails are fixedly installed on the inner walls of both sides of the mounting groove. A sliding plate is slidably connected to the slide rail, and the sides of the two sliding plates close to each other are respectively connected with a first mounting plate and a second mounting plate, and the bottom sides of the first mounting plate and the second mounting plate are respectively provided with a second mounting plate. A moving port and a second moving port, the first moving port is slidably connected with a connecting plate. The invention is easy to operate. By placing the controller on the first mounting plate and the second mounting plate, and then pulling the connecting plate, the connecting plate and the fixed column are clamped, and under the action of the tension spring, the two L-shaped The clamp clamps the controller, and then under the action of the torsion spring, the controller can be effectively damped to avoid problems with the controller and damage to the drone body.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a flight stability control system and method for an unmanned aerial vehicle. Background technique [0002] UAV is an unmanned aerial vehicle. UAV adopts high-tech such as satellite positioning, remote sensing, geospatial space, aerospace, automatic control, computer-aided analysis, etc. It can serve many fields such as land, surveying and mapping, forestry, transportation, water conservancy and military. In this field, the announcement number: CN105807779A discloses a UAV flight control system and method. The system includes an MCU central control module, an airborne sensor module, a data recording and export storage module, and a flight status indication module. The control method includes the following steps: 1. The airborne sensor module is used to collect data and transmit it to the MCU central control system through the CAN bus; 2. The MCU central control sy...

AI Technical Summary

Problems solved by technology

[0003] In this invention, there is no device for fixing and shock-absorbing the controller. The conventional UAV controller is basically installed with a bolt-fixed device, so when using a UAV, it will be easy Under the influence of its own vibration, the controller is damaged and the UAV is damaged. Therefore, we propose a UAV flight stability control system and method to solve the above-mentioned problems.

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