"Fuzzy Control of Rigid Spacecraft Attitude maneuver with decay Rate and ..."

Xihai Zhang, Ming Zeng, Xiao Yu (2011)

> Home

Details and statistics

DOI: 10.1142/S0218488511007453

access: closed

type: Journal Article

metadata version: 2022-05-23

- view
  - electronic edition via DOI
  - unpaywalled version
  authority control:
- export record
  dblp key:
  - journals/ijufks/ZhangZY11
- ask others
- share record
  persistent URL:
  - https://dblp.org/rec/journals/ijufks/ZhangZY11
Xihai Zhang, Ming Zeng, Xiao Yu:
Fuzzy Control of Rigid Spacecraft Attitude maneuver with decay Rate and Input Constraints. Int. J. Uncertain. Fuzziness Knowl. Based Syst. 19(6): 1033-1046 (2011)

manage site settings

To protect your privacy, all features that rely on external API calls from your browser are turned off by default. You need to opt-in for them to become active. All settings here will be stored as cookies with your web browser. For more information see our F.A.Q.