Advanced guidance algorithms for spacecraft formation-keeping

Proceedings of the American Control Conference

Volumn 4, Issue , 2002, Pages 2830-2835

  Tillerson, Michael ^a   How, Jonathan P ^a  

^a MASSACHUSETTS INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; COMPUTER SIMULATION; LINEAR PROGRAMMING; LINEARIZATION; MATHEMATICAL MODELS; OPTIMAL CONTROL SYSTEMS; ROBUSTNESS (CONTROL SYSTEMS); SPACECRAFT;

FORMATION FLYING CONTROL; SPACECRAFT FORMATION KEEPING;

ELECTRONIC GUIDANCE SYSTEMS;

EID: 0036058469     PISSN: 07431619     EISSN: None     Source Type: Journal    
DOI: 10.1109/ACC.2002.1025218     Document Type: Article

References (18)

1. Enabling spacecraft formation flying through spaceborne GPS and enhanced autonomy technologies
2. Formation flying experiments on the orion-emerald mission
3. TechSat 21 factsheet page
4. Mitigation of differential perturbations in synthetic apertures comprised of formation flying satellites
5. Geometry and control of satellite formations
6. 2 invariant relative orbits for spacecraft formations
7. Relative dynamics and control of spacecraft formations in eccentric orbits
8. Control of satellite formation
9. Coordination and control of distributed spacecraft systems using convex optimization techniques
10. Optimal trajectories for space navigation
11. Formation flying control in eccentric orbits
12. Satellite formation keeping control design based on ultimate bounded analysis of switched systems
13. Analysis of the impact of sensor noise on formation flying control
14. Project orion-emerald: Carrier differential GPS techniques and simulation for low earth orbit formation flying