Non-Singular and Continuous Back-Stepping Predefined-Time Attitude Tracking Control for Rigid Spacecraft with Predefined Bound
Author:
Affiliation:
1. Taiyuan Satellite Launch Center,Taiyuan,China,030045
2. Harbin Institute of Technology,Research Center of Satellite Technology,Harbin,China,150001
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9968313/9968303/09968880.pdf?arnumber=9968880
Reference22 articles.
1. Finite-Time Output Feedback Attitude Tracking Control for Rigid Spacecraft
2. Distributed Finite-Time Formation Control of Multi-Quadrotor Based on Leader-following Structure
3. Distributed finite-time attitude tracking control for modular spacecraft systems
4. Fixed-time attitude control for spacecraft without unwinding
5. Fixed-Time Attitude Tracking Control for Spacecraft With Input Quantization
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