Potential-function guidance forming eccentricity separation of satellites with continuous thrust

Transactions of the Japan Society for Aeronautical and Space Sciences

Volumn 44, Issue 144, 2001, Pages 127-129

  Umehara, H ^a  

^a NATIONAL INSTITUTE OF INFORMATION AND COMMUNICATIONS TECHNOLOGY   (Japan)

Author keywords

Artificial Satellites; Co Location; Formation Flight; Interaction; Orbit Control

Indexed keywords

AERODYNAMICS; COMPUTER SIMULATION; EQUATIONS OF MOTION; PERTURBATION TECHNIQUES; TRAJECTORIES;

POTENTIAL-FUNCTION GUIDANCE;

GEOSTATIONARY SATELLITES;

EID: 0035428835     PISSN: 05493811     EISSN: None     Source Type: Journal    
DOI: 10.2322/tjsass.44.127     Document Type: Article

References (8)

1. On the collision hazard of colocated geostationary satellites
2. Eccentricity separation of geostationary satellites using imaginary-interaction guidance
3. Improvement of eccentricity-inclination separation using imaginary-interaction guidance
4. On the co-location of eight ASTRA satellites
5. Autonomous ring formation for a planar constellation of satellites
6. The autonomous configuration of satellite formations using a generic potential function
7. Clustering motions in N-body systems - Free fall motions in the gaussian three-body problem