"Adaptive actuator failure compensation design for spacecraft attitude control."

Xuelian Yao et al. (2016)

> Home

Details and statistics

DOI: 10.1109/TAES.2016.130802

access: closed

type: Journal Article

metadata version: 2020-04-16

- view
  - electronic edition via DOI
  - unpaywalled version
  authority control:
- export record
  dblp key:
  - journals/taes/YaoTMQ16
- ask others
- share record
  persistent URL:
  - https://dblp.org/rec/journals/taes/YaoTMQ16
Xuelian Yao, Gang Tao, Yajie Ma, Ruiyun Qi:
Adaptive actuator failure compensation design for spacecraft attitude control. IEEE Trans. Aerosp. Electron. Syst. 52(3): 1021-1034 (2016)

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.