Intelligent attitude and orbit control system based on air-breathing electric propulsion

An electric propulsion, air-breathing technology, applied in the field of attitude and orbit control system, can solve the problem of not being able to work for a long time, and achieve the effects of avoiding waste of working fluid, prolonging service life and improving feasibility.

Inactive Publication Date: 2021-03-30
NAT UNIV OF DEFENSE TECH
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  • Abstract
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  • Claims
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Problems solved by technology

[0006] Aiming at the problem that the satellite jet attitude control system cannot work for a long time due to the limited fuel carried by the satellite, the invention provides an air-breathing-based electric propulsion, which collects the orbital atmosphere as the working medium, and then controls the actual working medium flow through the intelligent controller. An intelligent attitude-orbit control system that adjusts the supply of working fluid according to the demand of high-speed, and completes tasks such as attitude adjustment and orbit transfer while avoiding the waste of working fluid

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  • Intelligent attitude and orbit control system based on air-breathing electric propulsion
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  • Intelligent attitude and orbit control system based on air-breathing electric propulsion

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Embodiment Construction

[0038] The following will clearly and completely describe the technical solutions in the embodiments of the present invention in conjunction with the accompanying drawings in the embodiments of the present invention, and give further detailed descriptions, but the embodiments of the present invention are not limited thereto.

[0039] The application background of the present invention is an orbit at a height ranging from 150km to 250km. The atmosphere in this altitude range is basically in a free molecular flow state, and the density of the atmosphere decreases as the orbit increases.

[0040] Technical scheme of the present invention is:

[0041]The intelligent attitude and orbit control system based on air-breathing electric propulsion consists of an atmospheric absorption module 1, an intelligent adjustment module 2, an attitude and orbit control module 3, an energy supply module, a resistance compensation module 5 and an attitude execution module 6.

[0042] The air absorp...

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Abstract

The invention discloses an intelligent attitude and orbit control system based on air-breathing electric propulsion, and belongs to the field of spacecraft attitude and orbit control. The system is composed of an atmosphere absorption module, an intelligent adjustment module, an attitude and orbit control module, an energy supply module, an attitude execution module and a resistance compensation module. Atmospheric molecules in an orbit space are absorbed as a working medium, and then working medium supply is adjusted through the intelligent adjustment module according to the actual working medium flow rate requirement so as to support a pulse plasma thruster in the attitude execution module to carry out attitude adjustment and support a Hall thruster in the resistance compensation moduleto carry out resistance compensation and orbit transfer work. Solar panels are attached to the periphery of the system, and charging is conducted by absorbing solar energy so as to provide electric energy for all parts needing electric energy in the system. The system has the advantages that under the condition that a satellite carries a small number of working medium or even does not carry the working medium, absorbed atmosphere serves as the working medium to support various thrusters to carry out attitude adjustment and orbit transfer tasks, and working medium waste is avoided through intelligent adjustment.

Description

technical field [0001] The invention belongs to the field of attitude and orbit control of spacecraft, and specifically relates to a kind of low-carrying or even no-carrying working medium, which collects the orbital atmosphere as the working medium, and then adjusts the actual working medium flow rate requirements through intelligent control to meet the attitude adjustment and orbital requirements. Attitude and orbit control system for transfer requirements. Background technique [0002] In recent years, the number of space satellite launches has been increasing year by year. Only counting the launch plans that have been announced so far, tens of thousands of satellites will be launched in the next 10 years. However, the space orbit is a limited and non-renewable important resource. Considering that the number of satellites on the space orbit is becoming more and more saturated, in order to expand the operating range of the satellite and improve the mission capability of th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/24B64G1/40B64G1/36
CPCB64G1/242B64G1/36B64G1/405B64G1/244
Inventor 王昊义吴建军张宇程玉强李健赵元政谭胜欧阳郑鹏吴必琦崔星
Owner NAT UNIV OF DEFENSE TECH
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