Propellant-free Spacecraft Relative Maneuvering via Atmospheric Differential Drag
Abstract
Lyapunov Control: Controller signal is chosen such that: Lyapunov function of the tracking error is positive. Derivative of the Lyapunov function is negative. Thus ensuring that the tracking error converges to zero.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 2012
- Accession Number
- ADA568112
Entities
People
- Riccardo Bevilacqua
Organizations
- Rensselaer Polytechnic Institute