Integrated Power, Attitude, and Vibration Control of Gyroelastic Body

Chuandong Guo, Quan Hu*, Yao Zhang, Jun Zhang, Gongjun Li

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

3 Citations (Scopus)

Abstract

Gyroelastic body refers to a flexible structure with distributed angular momentum exchange devices, such as variable speeds control moment gyros (VSCMGs). A VSCMG contains a rotor with high rotating speeds. The direction and the magnitude of the rotor's angular momentum can be simultaneously tuned.When distributing a set of VSCMGs on a flexible structure, they could simultaneously produce control torques for attitude control and modal forces for vibration suppression. Meanwhile, the high spinning rotor in the VSCMGs can be used for energy storage. Thus, an integrated power, attitude, and vibration control system (IPAVCS) for a free flexible structure can be obtained. In this work, the control scheme for the IPAVCS is developed. A nonlinear controller is first designed to calculate the desired attitude control torques and vibration suppression modal forces for attitude stabilization and vibration suppression. Then, a robust pseudoinverse gimbal steering law and a pseudoinverse rotor acceleration law are developed to generate the desired control input and meet the power requirement, respectively. Numerical examples are conducted to verify the effectiveness of the proposed control scheme.

Original languageEnglish
Pages (from-to)3613-3623
Number of pages11
JournalIEEE Transactions on Aerospace and Electronic Systems
Volume58
Issue number4
DOIs
Publication statusPublished - 1 Aug 2022

Keywords

  • Attitude control
  • and vibration control system (IPAVCS)
  • attitude
  • energy storage
  • integrated power
  • variable speeds control moment gyros (VSCMGs)
  • vibration suppression

Fingerprint

Dive into the research topics of 'Integrated Power, Attitude, and Vibration Control of Gyroelastic Body'. Together they form a unique fingerprint.

Cite this