Fuel battery and storage battery hybrid power system energy management test platform and method thereof

A fuel cell system and hybrid power system technology, applied in the direction of measuring electricity, measuring electrical variables, measuring devices, etc., can solve the problems of difficult implementation, high risk, and high cost of flight test, and achieve low risk, improved efficiency, and low test cost Effect

Inactive Publication Date: 2017-11-24
BEIJING INSTITUTE OF TECHNOLOGYGY
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  • Abstract
  • Description
  • Claims
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Problems solved by technology

[0005] Aiming at the lack of a fuel cell battery hybrid unmanned aerial vehicle energy management strategy feasibility verification platform in the prior art, and the problems of high cost, high risk, and difficult implementation of real flight tests, the present invention discloses a fuel cell battery h

Method used

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  • Fuel battery and storage battery hybrid power system energy management test platform and method thereof
  • Fuel battery and storage battery hybrid power system energy management test platform and method thereof
  • Fuel battery and storage battery hybrid power system energy management test platform and method thereof

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Embodiment 1

[0039] Such as figure 1 As shown, this embodiment discloses an energy management test platform for a fuel cell battery hybrid power system, including a hybrid energy system, an energy management control system and a dynamic load simulation system. The hybrid energy system includes a hydrogen storage device, a flow meter, a fuel cell system, a storage battery and its plug; the energy management control system includes an energy management controller, a host computer, a voltage and current controllable DC / DC converter, and is used to monitor the storage battery The first current and voltage sensor and the second current and voltage sensor for monitoring the DC bus; the dynamic load simulation system is the programmable electronic load.

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Abstract

The invention discloses a fuel battery and storage battery hybrid power system energy management test platform and a method thereof, relates to an on-line energy management test platform and a method thereof and belongs to the unmanned aerial vehicle energy management and control technology field. A fuel battery and storage battery hybrid power system energy management test platform comprises a hybrid energy system, an energy management control system and a dynamic load simulation system. The hybrid energy system comprises a hydrogen storage apparatus, a flowmeter, a fuel battery system and a storage battery. The energy management control system comprises an upper computer, an energy management controller, a voltage and current controllable DC/DC converter and a current and voltage sensor. The dynamic load simulation system is a programmable electronic load. The invention also discloses a fuel battery and storage battery hybrid power system energy management test method based on the test platform. The invention aims at realizing feasibility verification of a fuel battery and storage battery hybrid power unmanned aerial vehicle energy management strategy and the advantages that test cost is low, a risk is small and realization is easy are possessed.

Description

technical field [0001] The invention relates to an online energy management test platform and method, in particular to an energy management algorithm verification platform and method for the fuel cell and storage battery hybrid power of an unmanned aerial vehicle, belonging to the technical field of energy management and control of unmanned aerial vehicles. Background technique [0002] New energy UAV is a new type of electric UAV with the potential of long-duration or even ultra-long-duration. It generally refers to the form of an energy system that uses fuel cells, solar cells, batteries and a variety of power sources mixed with each other. In view of the low energy density of batteries, generally pure battery UAVs have short flight time, and due to the soft discharge characteristics of fuel cells, pure fuel cells are not conducive to large-scale maneuvering flight and have poor anti-gust interference ability, while pure solar cells are unmanned. The aircraft is greatly af...

Claims

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Application Information

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IPC IPC(8): G01R31/36
CPCG01R31/3644
Inventor 刘莉张晓辉戴月领沈辉刘刚
Owner BEIJING INSTITUTE OF TECHNOLOGYGY
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