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A method and related device for adjusting satellite attitude

A satellite attitude and satellite model technology, applied in the field of satellite data processing, can solve problems such as gimbal lock, unfavorable imagination and observation, complex and cumbersome problems, etc., and achieve the effect of avoiding gimbal lock and intuitive adjustment methods

Active Publication Date: 2021-12-10
BEIJING GLOBAL CROWN JINYANG TECH DEV CO LTD
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Problems solved by technology

However, when the Euler angles are used to convert the left and right hands, the conversion formulas are different for different axes of the satellite model, and the method of using the Euler angles to adjust the satellite attitude is more complicated and cumbersome, and the gimbal lock is prone to occur. The problem cannot be easily solved; the quaternion represents a four-dimensional vector. For the three-dimensional vector of the satellite model, it is not intuitive enough to use the quaternion to adjust the satellite attitude, which is not conducive to imagination and observation

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  • A method and related device for adjusting satellite attitude
  • A method and related device for adjusting satellite attitude
  • A method and related device for adjusting satellite attitude

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Embodiment Construction

[0040] 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 a part of the embodiments of this application, not all of them. Based on the embodiments in this application, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the scope of protection of this application.

[0041] At present, after the satellite model corresponding to the satellite star switches the tangential mode, the ground mode, the sun mode, and the moon mode, etc., in order to keep the satellite attitude of the satellite model after switching modes is correct, the Euler angle is used to and / or quaternions to adjust the satellite attitude of the satellite model. ...

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Abstract

The present application discloses a method and a related device for adjusting the attitude of a satellite. The method includes: calculating the head-oriented target vector of the satellite model according to the Euler angle and the direction vector of the X-axis in the J2000 coordinate system; Adjust the head orientation of the satellite model and the head orientation target vector; calculate the sailboard orientation target vector of the satellite model according to the Euler angle and the orientation vector of the Y axis in the J2000 coordinate system; according to the current vector of the sailboard orientation of the satellite model and the sailboard orientation target Vector to adjust the orientation of the sails of the satellite model. Calculate the head-oriented target vector and the sailboard-oriented target vector of the satellite model. Based on the current head-oriented vector and the current sailboard-oriented vector of the satellite model, use the vector method to adjust the head-oriented and sailboard-oriented of the satellite model, which can shield the Disadvantages of adjusting satellite attitude by pull angle and / or quaternion; first adjust the head orientation of the satellite model and then adjust the sailboard orientation to effectively avoid gimbal lock.

Description

technical field [0001] The present application relates to the technical field of satellite data processing, and in particular to a method and a related device for adjusting satellite attitude. Background technique [0002] The satellite attitude refers to the space pointing state of the satellite body in orbit. The origin of the Cartesian coordinate system is located on the satellite body, the Z axis pointing to the ground reflects the yaw direction, the Y axis reflects the pitch direction, and the X axis reflects the roll direction. During the operation of the satellite body in orbit, it can switch between tangential mode, ground mode, sun mode, moon mode and other modes. axis, Y-axis and Z-axis, in order to keep the satellite attitude of the satellite model correct after switching modes, it is necessary to adjust the satellite attitude of the satellite model based on the offset of the X-axis, Y-axis and Z-axis . [0003] Generally, the Euler angles and / or quaternions ar...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/24G01C21/24
CPCB64G1/244G01C21/24
Inventor 张桥李京燕
Owner BEIJING GLOBAL CROWN JINYANG TECH DEV CO LTD