Impulsive feedback control to establish specific mean orbit elements of spacecraft formations

Journal of Guidance, Control, and Dynamics

Volumn 24, Issue 4, 2001, Pages 739-745

  Schaub, Hanspeter ^a   Alfriend, Kyle T ^b  

^a SANDIA NATIONAL LABORATORIES   (United States)

^b TEXAS A AND M UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EQUATIONS OF MOTION; FEEDBACK CONTROL; MATHEMATICAL MODELS; ORBITS; SENSITIVITY ANALYSIS; VARIATIONAL TECHNIQUES;

IMPULSIVE FEEDBACK CONTROL; MEAN ORBIT ELEMENTS; SPACECRAFT FORMATION FLYING;

SPACE FLIGHT;

EID: 0035394681     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4774     Document Type: Article

References (13)

1. Spacecraft formation flying: Dynamics and control
2. Along track formationkeeping for satellites with low eccentricity
3. Time-explicit representation of relative motion between elliptical orbits
4. Spacecraft formation flying control using mean orbit elements
5. Initial conditions and fuel-optimal control for formation flying of satellites
6. Mitigation of differential perturbations in clusters of formation flying satellites
7. 2 invariant reference orbits for spacecraft formations
8. Solution of the problem of artificial satellite theory without drag
9. GPS for low-cost attitude determination-A review of concepts, in-flight experiences, and current developments
10. Autonomous orbit determination for two spacecraft from relative position measurements
11. Small eccentricities or inclinations in the Brouwer theory of the artificial satellite