Optimal rendezvous in the neighborhood of a circular orbit
Abstract
The minimum velocity change rendezvous solutions, when the motion may be linearized about a circular orbit, fall into two separate regions; the phase-for-free region and the general region. Phase-for-free solutions are derived from the optimum transfer solutions, require the same velocity change expenditure, but may not be unique. Analytic solutions are presented in two of the three subregions. An algorithm is presented for determining the unique solutions in the general region. Various sources of initial conditions are discussed and three examples presented.
- Publication:
-
AIAA Conference on the Exploration of the Outer Planets
- Pub Date:
- July 1975
- Bibcode:
- 1975aiaa.confV....J
- Keywords:
-
- Circular Orbits;
- Satellite Orbits;
- Space Rendezvous;
- Trajectory Optimization;
- Transfer Orbits;
- Algorithms;
- Boundary Value Problems;
- Equations Of Motion;
- Linearization;
- Orbital Elements;
- Thrust Vector Control;
- Astrodynamics