TY  - RPRT
TI  - Momentum-Based Dynamics for Spacecraft with Chained Revolute Appendages
AU  - Queen, Steven
AU  - London, Ken
AU  - Gonzalez, Marcelo
PY  - 2005
UR  - https://ntrs.nasa.gov/citations/20050242042
ID  - 20050242042
ER  -