Improved Solution of Optimal Impulsive Fixed-Time Rendezvous
Abstract
A linear approach to the minimum-fuel problem of fixed-time multi-impulse rendezvous between vehicles on close circular orbits has proven to be simple and convenient. It deals with the linearized motion of the active vehicle relative to a reference point moving on a circular reference orbit. This paper shows that the normalized characteristic velocity is invariant with respect to each choice of reference orbit in the domain of normalized initial angular difference-normalized rendezvous time. Numerical examples are used to demonstrate the adaptability of linear solutions to the nonlinear case by means of a hybrid method. It is shown that the proposed mean velocity reference orbit more accurately describes the impulse locations and magnitudes than does the mean radius reference orbit.
- Publication:
-
Journal of Spacecraft and Rockets
- Pub Date:
- November 1982
- DOI:
- 10.2514/3.62295
- Bibcode:
- 1982JSpRo..19..521L
- Keywords:
-
- Circular Orbits;
- Fuel Consumption;
- Optimal Control;
- Orbital Rendezvous;
- Orbital Velocity;
- Equations Of Motion;
- Linearization;
- Specific Impulse;
- Time Dependence;
- Trajectory Optimization;
- Transfer Orbits;
- Astrodynamics