Satellite attitude data fusion system and method thereof

Patent metadata

Field	Value
Publication number	US-11046462-B2
Application number	US-201816234159-A
Country	US
Kind code	B2
Filing date	Dec 27, 2018
Priority date	Oct 18, 2018
Publication date	Jun 29, 2021
Grant date	Jun 29, 2021

Abstract

A satellite attitude data fusion system and method is disclosed, applicable to the earth satellite environment to estimate attitude data of the satellite. When the satellite attitude data fusion system of the present invention is used to perform the satellite attitude data fusion method, the first step is to perform a body rates quaternion attitude data processing operation. Then, the next step is to perform an attitude/rates data fusion processing operation, wherein an attitude data fusion algorithm module receives the first IAE result data from the first EKF, and the second JAE result data from the second EKF, and performs an attitude/rates data fusion algorithm in a subsystem level to evaluate an attitude estimation JAE performance.

First claim

What is claimed is:

1. A satellite attitude data fusion system, applicable to the earth satellite environment to estimate attitude data of the satellite, comprising:
a first EKF of a GS IAE;
a second EKF of the GS IAE;
a sensor;
a first gyro of a MEMS, wherein the first gyro of the MEMS is connected to the first EKF of the GS IAE;
a second gyro of a MEMS, wherein the second gyro of the MEMS is connected to the second EKF of the GS IAE; and
an attitude data fusion algorithm module,
wherein an attitude data fusion algorithm module, wherein the first gyro and the second gyro of the MEMS are connected to the attitude data fusion algorithm module, respectively,
wherein the first gyro and the second gyro of the MEMS are connected to the sensor, respectively,
wherein the first gyro of the MEMS performs a misalignment correction process and output first body rates data,
wherein the second gyro of the MEMS performs a misalignment correction process and output second body rates data,
wherein, the first EKF, the second EKF, the sensor, the first gyro, and the second gyro are used to perform a body rates quaternion attitude data processing operation based on the first body rates data, the second body rates data, and the quaternion attitude data to obtain first IAE result data and second IAE result data, and the attitude data fusion algorithm module performs an attitude/rates data fusion algorithm in a subsystem level to evaluate an attitude estimation IAE performance based on the first IAE result data, and the second IAE result data, and
wherein a first EKF of a GS IAE performs an first algorithm based on the first body rates data and the quaternion attitude data to obtain the first IAE result data, and a second EKF of the GS IAE performs an second algorithm based on the second body rates data and the quaternion attitude data to obtain the second IAE result data.

2. The satellite attitude data fusion system as claimed in claim 1 , wherein the first EKF of the GS IAE performs an first algorithm based on the first body rates data and the quaternion attitude data to obtain the first IAE result data, and the second EKF of the GS IAE performs an second algorithm based on the second body rates data and the quaternion attitude data to obtain the second IAE result data.

Assignees

• Nat Applied Res Laboratories

Inventors

• Jan Ying-Wei
• Yeh Ming-Yu
• Wei Wei-Ting
• Li Jia-Cheng
• Wu Yeong-Wei

Classifications

• G01C21/165

  combined with non-inertial navigation instruments · CPC title

• B64G1/36

  using sensors, e.g. sun-sensors, horizon sensors · CPC title

• B64G1/244 Primary

  Spacecraft control systems · CPC title

• B64G1/105

  Space science · CPC title

• G01C21/025

  with the use of startrackers · CPC title