"Attitude tracking control of rigid spacecraft with disturbance compensation."

Zhongtian Chen et al. (2019)

> Home

Details and statistics

DOI: 10.1504/IJMIC.2019.096838

access: closed

type: Journal Article

metadata version: 2020-09-17

- view
  - electronic edition via DOI
  - unpaywalled version
  authority control:
- export record
  dblp key:
  - journals/ijmic/ChenCTH19
- ask others
- share record
  persistent URL:
  - https://dblp.org/rec/journals/ijmic/ChenCTH19
Zhongtian Chen, Qiang Chen, Meiling Tao, Xiongxiong He:
Attitude tracking control of rigid spacecraft with disturbance compensation. Int. J. Model. Identif. Control. 31(1): 62-71 (2019)

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.