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Intelligent control system and method for multi-source hybrid power energy management of unmanned aerial vehicle

An intelligent control system and hybrid power technology, applied in the direction of power plant, aircraft parts, power plant type, etc. on the aircraft, can solve the problem of poor adaptability to the flight conditions of the UAV, avoid data transmission delay, and shorten development Cycle, the effect of fast transmission speed

Inactive Publication Date: 2020-11-17
天津轩云科技有限公司
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  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In view of this, the present invention provides a UAV multi-source hybrid energy management intelligent control system and method, which is applied to the UAV control system to solve the problem of poor adaptability to UAV flight conditions in the prior art. question

Method used

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  • Intelligent control system and method for multi-source hybrid power energy management of unmanned aerial vehicle
  • Intelligent control system and method for multi-source hybrid power energy management of unmanned aerial vehicle

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Embodiment Construction

[0028] In order to better understand the present invention, the present invention will be further described below in conjunction with specific embodiments and accompanying drawings.

[0029] The present invention provides an intelligent control system for UAV multi-source hybrid power energy management, which is used to control and energy manage the UAV multi-source hybrid power system; the UAV multi-source hybrid power system includes at least one engine and one ISG Start / generator integrated motor, in which the engine provides electric energy for the entire power system, which needs to meet the needs of UAV flight and airborne equipment power consumption, so the engine can be regarded as the power source of the entire UAV, so for the engine Control is critical.

[0030] Such as figure 1 As shown, the UAV multi-source hybrid energy management intelligent control system of the present invention at least includes a flight control system, an engine intelligent control system co...

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Abstract

The invention provides an unmanned aerial vehicle multi-source hybrid power energy management intelligent control system and method, and the system comprises a flight control system, an engine intelligent control system and an ISG starting / power generation integrated motor intelligent control system which are connected with the flight control system, and an intelligent energy distribution system.The engine intelligent control system is in communication connection with the engine, the ISG starting / power generation integrated motor intelligent control system is in communication connection withthe ISG starting / power generation integrated motor, and the intelligent energy distribution system is in communication connection with the engine intelligent control system and the ISG starting / powergeneration integrated motor. The unmanned aerial vehicle multi-source hybrid power energy management intelligent control system realizes overall control of the whole multi-source hybrid power system through mutual communication and cooperative work among the subsystems.

Description

technical field [0001] The invention relates to the technical field of multi-source hybrid power, in particular to an intelligent control system and method for multi-source hybrid power energy management of an unmanned aerial vehicle. Background technique [0002] The advantages of the hybrid electric propulsion system are low noise and reduced heat loss during operation, charging the battery during flight, allowing small internal combustion engines to be used in cruising conditions, serving as a backup energy source, realizing reverse motor start and restarting internal combustion engines in the air; The human-machine configuration hybrid electric propulsion system not only may increase flight time and reduce fuel consumption, but also can "stealth" complete surveillance tasks in pure electric mode, thereby greatly reducing engine noise and heat loss. [0003] For the designed hybrid electric propulsion system, it is necessary to design a control system that meets the usage...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D27/02B64D31/00
CPCB64D27/02B64D31/00B64D27/026
Inventor 宋玺娟朱敬锋岳峰飞李树花
Owner 天津轩云科技有限公司
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