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.
Propellant-free Spacecraft Relative Maneuvering via Atmospheric Differential Drag
2012
5 pages
Report
Keine Angabe
Englisch
Aerodynamics , Unmanned Spacecraft , Aerodynamic drag , Lyapunov functions , Spacecraft , Adaptation , Control , Errors , Flight , Functions , Maneuvers , Measurement , Numerical analysis , Onboard , Quadratic equations , Reduction , Signals , Symposia , Tracking , Briefing charts
Lyapunov-based adaptive feedback for spacecraft planar relative maneuvering via differential drag
Online Contents | 2014
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