Isolated satellite power source controller

A satellite power supply and isolated technology, which is applied in the field of isolated satellite power controllers, can solve problems such as lower bus voltage quality, achieve the effects of low bus output voltage stabilizing capacitors, improve bus voltage quality, and enhance adaptability

Inactive Publication Date: 2021-10-01
CHINA ELECTRONIC TECH GRP CORP NO 18 RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] Aiming at the deficiencies in the prior art, the present invention proposes an isolated satellite power controller, which is used to solve the problem of lower bus voltage quality of the traditional satellite power controller under the action of pulsating load, enhance the load adaptability of the power controller, and satisfy The power controller has strong adaptability and high-quality application requirements

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  • Isolated satellite power source controller
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Embodiment Construction

[0019] In order to enable those skilled in the art to better understand the solution of the present application, the technical solution in the embodiment of the application will be clearly and completely described below in conjunction with the accompanying drawings in the embodiment of the application. Obviously, the described embodiment is only It is an embodiment of a part of the application, but not all of the embodiments. Based on the embodiments in this application, all other embodiments obtained by persons of ordinary skill in the art without creative efforts shall fall within the scope of protection of this application.

[0020] It should be noted that the terms "comprising" and "having" and any variations thereof are intended to cover a non-exclusive inclusion, for example, a process, method, system, product or device comprising a series of steps or units is not necessarily limited to expressly instead of those steps or elements listed, may include other steps or eleme...

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Abstract

The invention discloses an isolated satellite power source controller, belonging to the technical field of satellite power source controllers. The isolated satellite power source controller is characterized by at least comprising: a solar cell power regulator connected with a solar cell array; a bus capacitor connected with a load; and an isolated storage battery charging and discharging regulator and a pulsating load, which are connected with a storage battery pack, wherein the positive electrode of the solar cell power regulator is connected with the negative electrode of the solar cell power regulator through the bus capacitor, the positive electrode of the isolated storage battery charging and discharging regulator is connected with the positive electrode of the solar cell power regulator, and the negative electrode of the isolated storage battery charging and discharging regulator is connected with the negative electrode of the solar cell power regulator. Due to the fact that a circuit of the isolated storage battery charging and discharging regulator is adopted, the load adaptability of the power source controller can be remarkably enhanced, and bus voltage quality is improved.

Description

technical field [0001] The invention belongs to the technical field of satellite power controllers, and in particular relates to an isolated satellite power controller. Background technique [0002] In the design of traditional satellite power controllers, in order to meet the power supply requirements of pulsating loads, the pulsating loads are usually directly connected to both ends of the battery pack, and the battery packs provide short-term high-power pulse power; for stable platform loads, connect To both ends of the bus capacitor, powered by the DC bus. Power supply block diagram as figure 1 As shown, the power controller is a non-isolated form, including a solar battery power regulator, a battery charge and discharge regulator, and a bus capacitor. The solar battery power regulator adjusts the output power of the solar battery array to generate a stable DC bus; the battery charge and discharge regulator charges the battery pack during the light period to ensure the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H02J7/35H02J1/10H02J7/00H02M3/335B64G1/42B64G1/44
CPCH02J7/35H02J1/10H02J1/106H02J7/0068H02J7/0063H02M3/33584B64G1/428B64G1/425B64G1/443H02J2207/20H02J2300/24Y02E10/56
Inventor 鲁伟王保平赵春阳陈洪涛孙宏杰张泰峰赵秋山代磊
Owner CHINA ELECTRONIC TECH GRP CORP NO 18 RES INST
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