Attitude control of a differentially flat underactuated rigid spacecraft

• Author / Creator

  Aguilar, César Octavio

• Subjects / Keywords

  • Space vehicles. Attitude control systems.
  • Feedback control systems.

• Graduation date

  2005

• Type of Item

  Thesis

• Degree

  Master of Science in Control Systems

• DOI

  https://doi.org/10.7939/r3-v2ch-e557

• License

  This thesis is made available by the University of Alberta Libraries with permission of the copyright owner solely for the purpose of private, scholarly or scientific research. This thesis, or any portion thereof, may not otherwise be copied or reproduced without the written consent of the copyright owner, except to the extent permitted by Canadian copyright law.