Nonlinear regulation for tracking and drag compensation of two-body spinning satellite

Journal of Guidance, Control, and Dynamics

Volumn 24, Issue 5, 2001, Pages 939-952

  Di Giamberardino, P ^a   Monaco, S ^a   Ronchini, R ^a  

^a SAPIENZA UNIVERSITY OF ROME   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; ASYMPTOTIC STABILITY; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; DRAG; ROBUSTNESS (CONTROL SYSTEMS); SATELLITES;

ATMOSPHERIC DRAG; LOW EARTH ORBIT SATELLITES;

NONLINEAR CONTROL SYSTEMS;

EID: 0035441679     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4801     Document Type: Article

References (13)

1. 'Galileo Galilei,' flight experiment on the equivalence principle with field emission electric propulsion
2. Galileo Galilei (GG), a small satellite to test the equivalence principle of Newton and Einstein
3. GALILEO GALILEI (GG)-test of the equivalence principle with a small spinning spacecraft: The stabilization of its weakly coupled masses
4. Experimental performance of field emission microthrusters
5. Evaluation of a proposed test of the weak equivalence principle using earth-orbiting bodies in high-speed co-rotation: Re-establishing the physical bases
6. On HALO orbits spacecraft stabilization
7. Orbit control for low-orbit recoverable satellite
8. Implementing autonomous orbit control
9. Drag-free control for ministep
10. Explicit guidance of drag-modulated aeroassisted transfer between elliptical orbits
11. Drag-free control systems and technologies