Optimal finite thrust rendezvous using beneficial effects of the earth oblateness

Advances in the Astronautical Sciences

Volumn 109 III, Issue , 2002, Pages 2497-2508

  Tebbani, Sihem ^a   Queinnec, Isabelle ^a   Bernussou, Jacques ^a  

^a LAAS CNRS   (France)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; EARTH (PLANET); OPTIMIZATION; ORBITS; QUADRATIC PROGRAMMING; SATELLITES;

EARTH OBLATENESS; OPTIMAL FINITE THRUST RENDEZVOUS;

SPACE RENDEZVOUS;

EID: 0036064504     PISSN: 00653438     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

1. Survey of numerical methods for trajectory optimization
2. Optimization of very-low-thrust many-revolution spacecraft trajectories
3. Optimal finite thrust orbit transfers with large numbers of burns
4. Station acquisition of a homogeneous constellation by linear and nonlinear optimization
5. Near circular orbital transfer optimization of impulsive thrusts
6. Quasi circular orbit transfer by means of impulsive thrusts
7. Low thrust orbit raising with coupled plane change and J2 regression
8. 2 regression
9. SQP-methods for solving optimal control problems with control and state constraints: Adjoint variables, sensitivity analysis and real-time control
10. Low thrust eccentricity and out-of-plane corrections
11. Trajectory-tracking guidance law for low-thrust Earth-orbit transfers