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Design of Attitude Control Actuators for a Simulated Spacecraft

Design of Attitude Control Actuators for a Simulated Spacecraft

Paperback

Technology & EngineeringGeneral Education

ISBN10: 1249613426
ISBN13: 9781249613428
Publisher: Biblioscholar
Published: Oct 10 2012
Pages: 192
Weight: 0.61
Height: 0.41 Width: 6.14 Depth: 9.21
Language: English

The Air Force Institute of Technology's attitude dynamics simulator, SimSat, is used for hardware-in-the-loop validation of new satellite control algorithms. To provide the capability to test algorithms for control moment gyroscopes, SimSat needed a control moment gyroscope array. The goal of this research was to design, construct, test, and validate a control moment gyroscope array for SimSat. The array was required to interface with SimSat's existing structure, power supply, and electronics. The array was also required to meet maneuver specifications and disturbance rejection specifications.

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