"Finite-time attitude tracking control for a rigid spacecraft using ..."

Lin Zhao, Yingmin Jia (2015)

> Home

Details and statistics

DOI: 10.1080/00207179.2014.996854

access: closed

type: Journal Article

metadata version: 2018-05-08

- view
  - electronic edition via DOI
  - unpaywalled version
  authority control:
- export record
  dblp key:
  - journals/ijcon/ZhaoJ15
- ask others
- share record
  persistent URL:
  - https://dblp.org/rec/journals/ijcon/ZhaoJ15
Lin Zhao, Yingmin Jia:
Finite-time attitude tracking control for a rigid spacecraft using time-varying terminal sliding mode techniques. Int. J. Control 88(6): 1150-1162 (2015)

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.