التفاصيل البيبلوغرافية
| العنوان: |
Attitude Maneuver Tests Using CMGs Mounted in a Three-Axis Free Dynamics Simulator. |
| المؤلفون: |
Takuya KANZAWA, Misuzu HARUKI, Tatsuya ENDO, Koji YAMANAKA |
| المصدر: |
Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan; 2016, Vol. 14 Issue ists 30, p7-13, 7p |
| مصطلحات موضوعية: |
GYROSCOPES, DYNAMIC models, FEEDBACK control systems, SINGULAR value decomposition, TORQUE control |
| مستخلص: |
This paper presents attitude maneuver demonstration tests using control moment gyroscopes mounted in a three-axis free dynamics simulator that provides an on-ground test environment of free rotational movement around three axes using the air-floating method. The issue of torque error between the torque command and the actual output torque is discussed in relation to the singularity-robust based steering law for spacecraft maneuvers. The torque error is analyzed using singular value decomposition to determine its magnitude and direction. Based on the analysis, feedback control and steering laws are proposed to reduce the torque error. Before conducting the maneuver demonstration test, a preliminary simulation is performed using a simplified dynamics model, control law, and steering law. The maneuver test results indicate that the dynamics simulator successfully accomplishes agile, large angle, and rest-to-rest multitarget maneuvers as well as precision pointing. [ABSTRACT FROM AUTHOR] |
|
Copyright of Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan is the property of Japan Society for Aeronautical & Space Sciences and its content may not be copied or emailed to multiple sites or posted to a listserv without the copyright holder's express written permission. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.) |
| قاعدة البيانات: |
Complementary Index |
