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Spacecraft attitude simulation control method and system

A spacecraft and attitude technology, which is applied in the field of spacecraft attitude simulation control method and system, can solve the problem that the quality of the control system cannot be judged intuitively.

Pending Publication Date: 2022-07-29
TIANJIN UNIV
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Problems solved by technology

[0003] In the process of realizing the disclosed concept, the inventors found at least the following problems in related technologies: the existing simulation control is based on digital simulation data and simulation curves, and it is impossible to intuitively judge the pros and cons of the current control system

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  • Spacecraft attitude simulation control method and system
  • Spacecraft attitude simulation control method and system
  • Spacecraft attitude simulation control method and system

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Embodiment Construction

[0054] Hereinafter, embodiments of the present disclosure will be described with reference to the accompanying drawings. It should be understood, however, that these descriptions are exemplary only, and are not intended to limit the scope of the present disclosure. In the following detailed description, for convenience of explanation, numerous specific details are set forth in order to provide a thorough understanding of the embodiments of the present disclosure. It will be apparent, however, that one or more embodiments may be practiced without these specific details. Also, in the following description, descriptions of well-known structures and techniques are omitted to avoid unnecessarily obscuring the concepts of the present disclosure.

[0055] The terminology used herein is for the purpose of describing particular embodiments only and is not intended to limit the present disclosure. The terms "comprising", "comprising" and the like as used herein indicate the presence o...

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Abstract

The invention provides a spacecraft attitude simulation control method and system, which can be applied to the technical field of spacecraft attitude control and simulation. The spacecraft attitude control simulation method comprises the steps that first attitude data are acquired from a target machine, the first attitude data are determined according to a spacecraft attitude maneuver control algorithm, and the first attitude data represent target data used for controlling a spacecraft model to display a target attitude; the first posture data are input into a turntable controller, second posture data are output, and the second posture data represent real-time data used for displaying the target posture; determining control deviation data according to the first attitude data and the second attitude data; and inputting the control deviation data into a turntable controller for controlling and displaying the target attitude of the spacecraft model.

Description

technical field [0001] The present disclosure relates to the technical field of spacecraft attitude control and simulation technology, and more particularly, to a method and system for spacecraft attitude simulation control. Background technique [0002] In order to ensure the stability of the spacecraft algorithm, a large number of simulation controls are often required to verify the stability of the spacecraft attitude control before the spacecraft test flight. During the simulation control, different verification devices need to be designed according to the spacecraft algorithm. [0003] During the process of realizing the concept of the present disclosure, the inventor found that there are at least the following problems in the related art: the existing simulation control is based on digital simulation data and simulation curves, and it is impossible to intuitively judge the pros and cons of the current control system. SUMMARY OF THE INVENTION [0004] In view of this,...

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Application Information

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IPC IPC(8): G05B17/02
CPCG05B17/02
Inventor 宗群殷梓元张秀云李智禹
Owner TIANJIN UNIV
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