Trajectory design strategies for the NGST L2 libration point mission

Advances in the Astronautical Sciences

Volumn 108 II, Issue , 2001, Pages 1465-1480

  Folta, David ^a   Cooley, Steven ^a   Howell, Kathleen ^a  

^a NASA GODDARD SPACE FLIGHT CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ASTRONOMY; COMPUTER AIDED DESIGN; FLIGHT DYNAMICS; MOTION CONTROL; SPACE RESEARCH; SPACE TELESCOPES; STATE SPACE METHODS; TRAJECTORIES;

COLLINEAR LIBRATION POINT; LIBRATION ORBIT CONTROL; NEXT GENERATION SPACE TELESCOPE; SOFTWARE PACKAGE ASTROGATOR; SOFTWARE PACKAGE SWINGBY; TRAJECTORY DESIGN;

SPACE FLIGHT;

EID: 0035734253     PISSN: 10816003     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

1. Application of dynamical system theory to trajectory design for a libration point mission
2. Trajectory design strategies that incorporate invariant manifolds and swingby
3. Mission design for a halo orbiter of the earth
4. The flight of ISEE-3/ICE: Origins, mission history, and a legacy
5. Transfer trajectory design for the SOHO libration point mission
6. Optimum transfer to a large-amplitude halo orbit for the Solar and Heliospheric Observatory (SOHO) spacecraft
7. Trajectory optimization for the ACE halo orbit mission
8. An interactive tool for design and support of lunar, gravity assist, and libration point trajectories
9. Formation flying with decentralized control in libration point orbits
10. Stationkeeping techniques for libration-point satellites
11. Accelerometer enhanced trajectory control for the ISEE-3 halo orbit
12. Biasing maneuvers for directional control of stationkeeping delta V's in libration point orbits
13. Investigation of the effects of maneuver uncertainties on a finite set of different controllers and maneuver strategies
14. Station-keeping method for libration point trajectories