A primary discussion for Mayer pattern of optimization orbitinjection problem
Abstract
This paper discusses two types of optimization of the orbitinjection problem. One is a minimumtime orbitinjection, and the other is a maximum radius of circular orbitinjection at a given time. Both of them are directed against orbitinjection from a point in space to an orbitplane to be presented. A new algorithm is established for solving these two problems which can be used to solve all types of twoboundary problems, including the problem of terminal constraints, the problem at an unspecified terminal time, and the hybrid of these two types and so on.
 Publication:

Chinese Society of Astronautics Journal
 Pub Date:
 July 1984
 Bibcode:
 1984ChSAJ.......85L
 Keywords:

 Computerized Simulation;
 Injection Guidance;
 Optimal Control;
 Orbital Mechanics;
 Trajectory Optimization;
 Algorithms;
 Boundary Value Problems;
 Equations Of Motion;
 Mayer Problem;
 Orbital Launching;
 Astrodynamics