Attitude control of spinning satellite subject to actuators restriction using eigenstructure assignment.

Details

Language :

English

ISBNs :

9780780393950

Database :

Complementary Index

Journal :

2006 1st International Symposium on Systems & Control in Aerospace & Astronautics

Publication Type :

Conference

Accession number :

80806320

Full Text :

https://doi.org/10.1109/ISSCAA.2006.1627503