control moment gyroscope, satellite attitude control, spacecraft maneuver, angular momentum, moment of inertia, bang-bang control, torque, reaction wheel, actuator
その他のタイトル（英）
A study of high performance maneuver for artificial satellite
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics
JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Satellite Systems
巻
JAXA-SP-05-008
ページ
219 - 224
発行年
2006-01-20
抄録（英）
This is the report of a study of high performance maneuver for artificial satellite. Especially, CMG (Control Moment Gyro) aiming to agile reorientation maneuver is discussed in this report. The number and the arrangement of the CMG cluster were examined, for Rest-to-Rest maneuvering. The performance presumption parameter to the first design estimate was derived. The CMG assembly design for agile maneuver is determined by requirement of angular momentum and the moment of inertia of satellite. The result of the CMG assembly arrangement should be discussed from the point of electrical energy consumption, precise weight estimation and cost.
人工衛星の高性能姿勢制御の研究
49054045.pdf
(1.3MB)
