| 摘要 |
<p>PROBLEM TO BE SOLVED: To overcome the disadvantages of architectures and methods for hybridizing data of various AOCS sensors used thus far.SOLUTION: A synchronization line 7 supplies a uniform time clock from a particular active central master processing unit out of a central master processing unit 2a or out of a redundant central processing unit 2b to another kinematic sensor 3, and connects the central master processing unit 2a and the redundant central processing unit 2b to a second bus 5 of a spacecraft, and via the connection, the particular active central processing unit 2a supplies the central computer 6 of the spacecraft with hybridized kinematic measuring data 8a, 8b composed of synchronized kinematic measuring data 23 of a star sensor and measuring data 24 of the other kinematic sensor.</p> |
