Unmanned-aerial-vehicle height measurement control system based on fault-tolerance processing and control method

Abstract

The invention discloses an unmanned-aerial-vehicle height measurement control system based on fault-tolerance processing and a control method. The unmanned-aerial-vehicle height measurement control system comprises a height meter module, a satellite navigation module, an inertial measurement module and a computing and processing module. The height meter module is used for measuring the distance of an unmanned aerial vehicle to the ground in real time; the satellite navigation module is used for receiving and processing satellite signals in real time and measuring the flight position and the direction of the unmanned aerial vehicle; the inertial measurement module is used for measuring the attitude angular velocity and the accelerated velocity of the unmanned aerial vehicle in real time; the computing and processing module is used for receiving data of the height meter module, the satellite navigation module and the inertial measurement module in a parallel mode and computing and obtaining height measurement data. By means of the unmanned-aerial-vehicle height measurement control system based on fault-tolerance processing and the control method thereof, the conditions of the fault of a height meter or the fault of satellite navigation or the faults of a height meter and satellite navigation can be synthetically processed, and the high stability of the unmanned aerial vehicle is guaranteed through the control system to a maximum limit.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicle navigation control, in particular to an unmanned aerial vehicle altitude measurement control system and control method based on fault-tolerant processing. Background technique [0002] The absolute altitude (ie altitude) of the unmanned aerial vehicle is an important parameter for the flight of the aircraft, and is a key parameter to be controlled when the cruise aircraft is flying. Stable and reliable real-time measurement of the absolute altitude of the aircraft (that is, the altitude) is the guarantee for determining the stability of the altitude control system of the unmanned aerial vehicle. The devices for measuring the altitude of the aircraft mainly include satellite navigation systems and altimeters. The satellite navigation system can work around the clock in open areas with high accuracy, but it is prone to loss of capture and abnormal operation when encountering obstructions. Alt...

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Problems solved by technology

[0005] Usually, the key to fault tolerance is redundancy. Redundancy in the prior art is generally achieved by adding additional hardware resources and additional software to achieve fault detection and fault tolerance. This often increases the cost of equipment and the algorithm is complex, which is reflected in the focus on The data fusion of multiple t

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