Grid flicker safety protection method and device of ion electric propulsion system and storage medium

A technology of propulsion system and ion electricity, which is applied in the direction of aerospace vehicle propulsion system devices, thrust reverse devices, and utilization of plasma, and can solve problems such as power supply and distribution safety, electromagnetic compatibility hazards, flight mission failures, and satellite failures. Achieve the effects of ensuring good operation, avoiding safety hazards, and improving on-orbit life

Active Publication Date: 2021-10-22
BEIJING INST OF CONTROL ENG
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  • Claims
  • Application Information

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Problems solved by technology

[0003]Grid flickering is an inherent working characteristic of ion thrusters, because it involves instantaneous short-circuit of high-voltage power supply, if there are no protective measures, it may affect the safety and security of the power supply and distribution of the entire star Electromagnetic compatibility poses a hazard, which may lead to satellite failure in severe cases
In the early on-orbit verification process of the foreign ion electric propulsion system, the mission failed due to the fault of the grid flicker of the ion electric propulsion system

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  • Grid flicker safety protection method and device of ion electric propulsion system and storage medium
  • Grid flicker safety protection method and device of ion electric propulsion system and storage medium
  • Grid flicker safety protection method and device of ion electric propulsion system and storage medium

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Embodiment Construction

[0020] The present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0021] In order to protect the grid flicker of the ion electric propulsion system from causing harm to the system and the whole star, the present invention designs a grid flicker safety protection method for the ion electric propulsion system.

[0022] For the grid scintillation characteristics of the ion electric propulsion system, the following technical problems need to be solved:

[0023] (1) According to the grid current variation characteristics when the grid flicker occurs during the ignition process of the ion electric propulsion system, a targeted grid flicker judgment condition is proposed;

[0024] (2) According to the inherent grid flicker characteristics of the ion electric propulsion system, formulate reasonable processing strategies, corresponding to mild flicker, moderate flicker and severe flicker respectively. Durin...

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Abstract

The embodiment of the invention provides a grid flicker safety protection method of an ion electric propulsion system. The method comprises the following steps that (1), the current grid current Ib of the ion electric propulsion system is monitored; and (2), if the current grid current Ib is greater than a first set threshold value, it is judged that the current grid current Ib is an overcurrent signal, when the duration of the overcurrent signal is less than or equal to the time t0, the step (1) is executed, when the duration of the overcurrent signal is greater than the time t1, the operation of adjusting the grid voltage and the grid current to be 0 in the step (3) is executed, and when the duration of the overcurrent signal is greater than the time t0 and less than or equal to the time t1, the judgment and the operation in the step (4) are executed. By utilizing the technical scheme provided by the embodiment, safety protection can be provided for the ion electric propulsion system on the premise of avoiding frequent and repeated starting, and on-orbit safe operation of a satellite is guaranteed.

Description

technical field [0001] The invention relates to a grid flicker safety protection method, device, storage medium and computer program product of an ion electric propulsion system, belonging to the technical field of ion electric propulsion system safety protection. Background technique [0002] Due to the high power, for example, the 5kW multi-mode ion electric propulsion system has the characteristics of high specific impulse and long life. Many large advanced satellites are equipped with this ion electric propulsion system. The maximum working voltage of the electrode reaches 1450V. Due to dust, sputtering deposits, grid burrs and other reasons, when the ion thruster is ignited, an instantaneous grid short circuit phenomenon is inevitably generated, which is called grid flicker. [0003] Grid flicker is an inherent working characteristic of the ion thruster, because it involves an instantaneous short circuit of the high-voltage power supply. If there are no protective measu...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F03H1/00B64G1/40
CPCF03H1/0087B64G1/405
Inventor 高俊邹达人李永何刚丁凤林李宗良韩亮丛云天郭盼高秀娟
Owner BEIJING INST OF CONTROL ENG
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