Power consumption controllable unmanned aerial vehicle flight control system and method

Abstract

The invention discloses a power consumption controllable unmanned aerial vehicle flight control system. The power consumption controllable unmanned aerial vehicle flight control system comprises a system module. The starting control end of the system module is connected with a control receiving end of a hardware drive module. The driving end of the hardware drive module is connected with the signal receiving end of a driver module. The control end of the driver module is connected with the starting end of a posture resolving module and a posture stabilizing module. The signal input end of the posture resolving module and the signal input end of the posture stabilizing module are connected with the collecting signal output end of a sensor module. The signal output end of the posture resolving module and the signal output end of the posture stabilizing module are connected with the signal input end of a controller module. The signal output end of the controller module is connected with the signal input end of a flight point module and the signal input end of a guidance module. The signal output end of the controller module is further connected with a load module, and a power module is used for supplying power to the whole system.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicle flight control, in particular to an unmanned aerial vehicle flight control system and method with controllable power consumption. Background technique [0002] A drone is an aircraft capable of autonomous flight. As an important part of the UAV, the flight control system's performance has a great impact on the overall technical and tactical indicators of the UAV system. In a certain sense, the flight control system has a narrow sense flight control system and a general sense flight control system. The so-called narrow sense flight control system refers to the inner loop stabilization loop and the outer loop position loop, including sensor modules, control algorithm modules and execution modules. , the system that completes the airframe control task is a pure control system; while the generalized flight control system also includes functions such as onboard electrical, load control...

AI Technical Summary

Problems solved by technology

However, the problem brought by this system is the high power consumption of the whole system

[0004] For another flight control system, the cost of the aircraft is low and generally does not need to operate cumbersome flight movements, so the flight control system it needs goes to another extreme, using cost-effective hardware and single-threaded software to control the aircraft to do General flight maneuvers, its power consumption is very low, but it reduces performance and reliability at the same time

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