Paper information
- Paper code
- Order
5
- Room
Salon Jalisco E6
- Title
Integrated 6-DOF spacecraft orbit-attitude dynamics modeling and its application in hovering control over an asteroid
- abstract
- Session
2. Guidance, Navigation & Control (2)
- symposium
C1. ASTRODYNAMICS SYMPOSIUM
- congress
IAC-16
- Type of presentation
oral
Dr. Yue Wang, Beihang University, China