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A Satellite Attitude Control System

A satellite attitude control and attitude control technology, which is applied in the directions of space navigation equipment, space navigation equipment, space navigation aircraft, etc., can solve the problem of not considering the difference in the design of satellite controllers, and not considering the collaborative work of multiple attitude control execution components and other problems to achieve the effect of improving reconfigurability and reliability

Active Publication Date: 2021-11-23
TSINGHUA UNIV
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0005] However, in the above-mentioned existing satellite attitude control methods, the difference in controller design of the satellite at different stages is not considered, and only one control strategy of the attitude control execution unit is described, and the coordination among multiple attitude control execution units is not considered. Work

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  • A Satellite Attitude Control System
  • A Satellite Attitude Control System
  • A Satellite Attitude Control System

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Embodiment Construction

[0034] Embodiments of the present application are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary, and are intended to explain the present application, and should not be construed as limiting the present application.

[0035] The following describes the satellite attitude control system of the embodiment of the present application with reference to the accompanying drawings.

[0036] figure 1 It is a schematic structural diagram of the satellite attitude control system proposed by the embodiment of the present invention. like figure 1 As shown, the satellite attitude control system proposed by the embodiment of the present invention mainly includes four functional modules, which are respectively a command processing module, an attitude d...

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Abstract

The present application proposes a satellite attitude control system, comprising: a command processing module, an attitude determination module connected to the command processing module, an attitude control module and an information storage module, wherein the command processing module is used for receiving, interpreting, discriminating and executing Control instructions from the ground station or the star management system; the attitude determination module is used to calculate the current attitude information of the satellite according to the measurement data collected by the attitude sensitive device in the preset control stage, and the attitude control module obtains the attitude information determined by the attitude determination module. , and according to the attitude information, calculate according to the control law corresponding to the preset control stage, generate the control command of the attitude control actuator, and drive the attitude control actuator to execute the control command; the information storage module is used to store the information and attitude of the attitude sensitive device. The information of the actuator is controlled, and the stored information is composed of the whole orbit data package and transmitted to the ground station. The present application satisfies the attitude control requirements of satellites at various stages.

Description

technical field [0001] The invention relates to a satellite attitude control system (Attitude Determination and Control System, ADCS), belonging to the technical field of spacecraft attitude control. Background technique [0002] Satellite attitude control system is an important part of the whole satellite system. The attitude control system is an embedded real-time control system. It is different from the general control system, its composition is complex, and its reliability is high. The attitude control system specifically includes satellite body dynamics analysis, attitude sensors, attitude determination algorithms, attitude control algorithms, and actuators. [0003] The design goal of attitude control system software, like all software designs, is to meet the requirements to the maximum extent under the constraints of time and various resource environments. The on-orbit operating environment of the attitude control system is constantly changing. The software design ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/24
CPCB64G1/244
Inventor 孟子阳孙晓龙张高飞
Owner TSINGHUA UNIV
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